Negli ultimi tempi, costruire un aquilone è un'arte esclusiva di
un piccolo gruppo di persone che sono dotate di grandi conoscenza aerodinamiche,
abilità nel disegno, nel cucire e altre abilità manuali.
Non più! Con l'aiuto di moderni programmi software per
progettare aquiloni, database di airfoils, esempi di progetto di aquiloni e
aiuti esterni per le cuciture, quasi tutti i kiters possono farsi il loro
aquilone costruito su misura. Lasciateci guardare questi elementi uno ad uno per
vedere dove siamo arrivati con l'arte di costruirsi il proprio aquilone:
Gli aquiloni sono dispositivi aerodinamici veramente complessi (complessi
quanto un'ala di aereo se non di più). Se non avete confidenza con termini
come airfoil, profilo, ala e altra terminologia associata, leggete
http://www.dreesecode.com/other/aflprimer.pdf o altre premesse sugli prima
di continuare.
I parametri più facili da maneggiare e altamente visibili sono
l'Aspect Ratio (AR), l'Airfoil Profile e l'Angolo di attacco (AoA) dell'aquilone:
Aspect Ratio
Aspect Ratio è approssimativamente l'Larghezza/Corda
dell'aquilone o più precisamente Larghezza*Larghezza/Area. Finchè lo AR determinerà
la forma dell'aquilone questo saràl'aspetto più visibile da parte
dell'utilizzatore. Aquiloni con alto AR hanno meno trascinamento indotto (up-wash
e effetto vortice sui tip) rispetto ad aquiloni con le stesse
caratteristiche ma basso AR. Il trascinamento indotto è inversamente
proporzionale allo AR. Quando sono stazionari nella finestra del vento, un
aquilone con basso
AR può generare la stessa quantità di trazione di uno con alto AR (con le stesse
caratteristiche) ma come abbiamo bisogno di muovere l'aquilone (per saltare o in
condizioni di scarsa potenza), un aquilone con alto AR può accelerare più
velocemente e quindi prendere potenza più velocemente di un aquilone con basso
AR. Come regola generale, un alto AR indica una finestra di potenza più
grande (la differenza tra la minima e la massima potenza) a un basso AR una più
piccola. Di seguito si riportano i valori di AR consigliati:
Aquilone
AR molto basso
AR basso
AR moderato
AR alto
AR molto alto
Foil
2.5-
3
4
5
5.5+
Gonfiabile / Arc
3-
4
5
6
7+
I gonfiabili e l'Arc hanno una sagoma sferica, una forma
naturale stabile, il loro AR è normalmente più alto di quello di un foil.
Profilo di Airfoil
Airfoil da sollevamento e trascinamento. Un profilo con
alto sollevamento quando stazionario alla finestra del vento da la massima
trazione (AoA circa 5 gradi). Un profilo con più alto rapporto
sollevamenbto trascinamento accelererà più velocemente e genererà più potenza
quando volerà attraverso la zona di potenza della finestra del vento. Un airfoil
con grande lift è talvolta etichettato come "trattore" perchè tira
come un trattore quando nella finestra del vento. Un aquilone con alto
rapporto sollevamento/trascinamento è etichettato come airfoil "veloce"
perchè vola molto veloce nella zona di potenza generando una tremenda potenza.
Un airfoil "veloce" può generare molta potenza nella finestra del vento ma non
necessariamente quanta ne genera un "trattore". La tabella successiva
mostra il raccomandato sollevamento e rapporto sollevamento/trascinamento:
Molto basso
Basso
Moderato
Alto
Molto alto
Coefficiente di sollevamento (at AoA = 5)
< 0.5
0.7
0.9
1
> 1.1 (trattore)
Rapporto Sollevamento/trascinamento
< 50
70
90
100
> 110 (veloce)
E' meglio usare un programma di progettazione di airfoil (come DesignFoil
su http://www.dreesecode.com/ - se
volete comprare il software dopo aver esaurito il periodo di prova, potete
ottenere uno sconto con la licenza educazionale menzionando che siete un lettore
della kitesurfingschool.org) per progettare, analizzare e selezionare il profilo
di aquilone da usare per il vostro airfoil (ai fini del kiting, in numero di Reynolds
va da 1.000.000 a 2.000.000).
Alcuni progettisti di aquiloni si vergognano della complessità del progetto,
dell'analisi e dell'uso delle regole comuni e dei metodi di cambiare lo spessore
del profilo per cambiarne le caratteristiche di sollevamento ed il rapporto
sollevamento/trascinamento. Questo metodo non è accurato ma per un
aquilonista può essere accettabile. A regola di bazzi'a, aumentare lo spessore
del profilo per aumentare il sollevamento alla finestra del vento e diminuire lo
spessore per aumentare la sua velocità. La tabella seguente mostra il
campo degli spessori dei profili più usati per gli aquiloni:
Profilo per Foil e Arc
Profilo per Gommoni
sottile (veloce):
< 14%
moderato: 15%
spesso: 16%
molto spesso: 17%
il più spesso
(trattore): 18% or more
sottile (veloce): 8%
- 9%
moderato: 10%
spesso: 11%
molto spesso: 12%
il più spesso
(trattore): 13% - 14%
AoA a tipico
Un aquilone ha più
sollevamento con alto Angolo di Attacco (AoA) al vento (più superficie
proiettata al vento e anche un AoA da 0 a 16°, il Coeficiente di sollevamento di
un airfoil aumenta ad un valore ottimale). Ciascun aquilone ha un suo AoA
tipico e "neutro" per il suo centro e per le sue estremità quando è in
sopra la vostra testa al limite della finestra del vento
(con le linee di potenza e dei freni della stessa lunghezza). L' AoA
tipico, in condizioni quindi di riposo, va da 0 a 5 gradi. Occorre notare
che a riposo l'aquilone vola a 85° di elevazione in modo che l'AoA del centro
del profilo in volo è la somma dello AoA tipico e la differenza tra l'elevazione
di volo dell'aquilone e la verticali (5 gradi ottenuti come 90 - 85°).
Cambiando l'AoA tipico può cambiare la dimensione della finestra del vento tanto
che le due possono "amplificare" ciascuna l'altra per avere un effetto
di "doppio AoA".
Per es. cambiando lo AoA tipico da 2 a 0 fa cambiare la finestra del vento da 85
a 84°; quindi l'AoA dell'aquilone in volo alla finestra del vento è 4° invece di 7.
E' interessante leggere i Miti di
Peter
Lynn 1 e 2 in cui egli inizia dicendo che il sollevamento o trazione
dell'aquilone alla finestra del vento è proporzionale alla AoA tipica mentre il
rapporto sollevamento/trascinamento è inversamente proporzionale. [sebbene l'aquilonista
possa cambiare l'AoA dell'aquilone durante il volo cambiando la lunghezza delle
linee frontali rispetto a quelle posteriori, comunque, questo in qualche modo
deforma l'aquilone facendogli perdere alcune delle caratteristiche che si
volevano raggiungere in sede di progetto. Un aquilone lavora meglio con un AoA
intorno a quello di progetto]
un aquilone con un
basso AoA ha una finestra del vento maggiore ma può sovravolare (passarci sopra
la testa,, oltre i 90°) e collassare facilmente senza avere molta trazione alla
finestra del vento (un aquilone veloce dovrebbe avere un AoA basso, intorno a 0°).
Questo tipo di aquilone deve avere un controllo istantaneo dell'AoA per
prevenire collassi e anche per poter dare al kiter più potenza al bordo della
finestra del vento.
un aquilone con un
alto AoA ha una finestra del vento più piccola ma genera più trazione alla
finestra del vento ed è più difficile che collassi (un trattore può avere unAoA
da 3 a 5° per una maggiore trazione alla finestra del vento)
un aquilone tutto
fare dovrebbe avere un AoA da 2 a 3°.
a causa dei fenomeni
di up-wash e dei vortici all'estremità dell'ala, l'AoA delle estremità dell'ala
può essere di 1 o 2 ° superiore dell' AoA a centro ala. L'effetto di wash-up
riduce l' AoA all'estremità dell'ala, tale effetto può essere compensato
progettando un aquilone con un AoA alle estremità più alto di 1 o 2° rispetto al
centro.
per i gonfiabili e l' Arc,
a causa della loro geometria, l'AoA all'estremità delle ali varia molto rispetto
all'AoA del centro e quindi i due AoA sono progettati indipendentemente e il
progettista deve aggiungere 1 o 2° al desiderato AoA per compensare l'effetto
dei fenomeni di up-wash e dei vortici all'estremità dell'ala.
AoA molto basso
AoA basso
AoA moderato
AoA alto
AoA molto alto
Campo (in gradi)
< 0
1
2 - 3
4
> 5
Tipo di aquilone
corsa
velocità
tutto fare
onde
trattore (Wake Style)
La tabella seguente fornisce il sommario dei parametri della AR, Airfoil, AoA:
Basso
Alto
AR
piccola finestra di potenza
grande finestra di potenza
sollevamento (alla finestra del
vento)
perdite di trazione alla finestra del vento
forte trazione alla finestra del vento
rapporto sollevamento/trascinamento
lento
veloce
AoA tipica a riposo
grande finestra del vento
piccolo AoA alla finestra del vento (meno trazione)
collassa facilmente
veloce
piccola finestra del vento
alto AoA alla finestra del vento (maggiore trazione)
difficile da collassare
lento
ed il loro uso in differenti tipi di aquilone:
Tipo aquilone/vento
vento leggero
(6 - 15 nodi)
vento moderato
(12 - 27 nodi)
vento forte
(> 27 nodi)
Gonfiabili (Foil)
16 m2 (10 m2) e oltre
8 - 16 m2 (5 - 10 m2)
8 m2 (5 m2) e più piccoli
Scuola (stabile, basso sollevamento,
lento)
moderato AR
buon sollevamento
buon sollevamento/trascinamento
moderato AoA
basso AR
basso Lift
moderato - basso sollevamento/trascinamento
basso AoA
molto basso AR
molto basso Lift
molto basso sollevamento/trascinamento
moderato - basso AoA
Trattore (Wake Style,
onde, vento a raffica)
moderato AR
elevato sollevamento
buon sollevamento/trascinamento
alto AoA
moderato - basso AR
buon sollevamento
moderato Lift/trascinamento
alto - molto alto AoA
basso AR
moderato Lift
basso sollevamento/trascinamento
moderato - High AoA
Tutto fare
alto AR
buon sollevamento
elevato sollevamento/trascinamento
alto AoA
moderato AR
moderato Lift
alto - moderato sollevamento/trascinamento
basso AoA
elevato AR
buon sollevamento
elevato sollevamento/trascinamento
moderato - basso AoA
alto AR
moderato Lift
buon sollevamento/trascinamento
basso - molto basso AoA
moderato AR
basso sollevamento
moderato - basso sollevamento/trascinamento
basso AoA
Altri fondamenti sulla progettazione
il centro del profilo
va selezionato per un ottimale sollevamento e per un ottimo rapporto
sollevamento/trascinamento (ottimo in accordo con la tabell aprecedente sull
abase delle caratteristiche richieste all'aquilone da progettare)
il profilo dell
eestremità dell'ala va selezionato per la massima resistenza al collasso
dell'ala
(es. profilo reflex)
per i gonfiabili o per
l'Arc:
questi aquiloni hanno
la "stessa" superficie proiettata del 63% (2/p o
2/3.14159) della superficie della vela rispetto a qualsiasi altro parametro
dell'aquilone (AR, rapporto bordo/centro corda, ecc.)
se le estremità
dell'ala sono abbastanza grandi (il punto di rimorchio effettivo delle linee
posteriori è più grande dell'80% della corda centrale), si può fare il rilancio
all'indietro dell'aquilone tirando sulle linee posteriori
se le estremità dell'ala
sono grandi abbastanza e l'effettivo punto di rimorchio è meno del 15% della
corda centrale, l'aquilone non volerà da solo con la sola linea frontale (100% depower)
Ulteriori informazioni sulla progettazione
degli aquiloni
Molti progettisti di aquiloni o software di progettazione di
foil vengono forniti con una raccolta dati; comunque potreste volere di più, ci
sono alcune raccolte di dati sugli airfoil ed una delle più grandi è
UIUC Airfoil Coordinates Database.
Il più popolare programma software per il progetto di
aquiloni gonfiabili è SurfPlan (Surf sta per Surface = Superficie). SurfPlan
è scaricabile al sito http://www.surfplan.com.au/.
Il programma SurfPlan non ha ancora un manuale ufficiale.
Comunque Kitesurfingschool.org ha uno "Pseudo"
manuale dell'utente di Surfplan alla fine di questa pagina [se ci sarà
abbastanza domanda, KitesurfingSchool.Org proverà, in futuro, a scrivere una
versione completa del manuale SurfPlan - lasciatecelo sapere]. C'è anche un manuale
in francese per un avecchia versione 3.4
di SurfPlan (dell'aprile 2005 e l'attuale versione di SurfPlan è la 4.5) su
http://perso.wanadoo.fr/orveillon/manuel/manuel-1.htm.
I progettatori di foil potranno usare FoilMaker che era in giro
prima di
Surfplan ed è molto popolare tra gli entusiasti dei foil. FoilMaker può
essere scaricato da
http://www.foilmaker.co.uk/.
FoilMaker ha un suo manuale dell'utente e il sito web mostra alcuni esempi di
progettazione di aquiloni.
Il proprietario del sito web ha fatto un magnifico lavoro
lavoro fornendo gli esempi di progetto di vari aquiloni da cui imparare
per farsene. All'inizio, è consigliabile prendere in
considerazione pochi parametri semplici come:
Colore
Dimensioni
Aspect Ratio (non cambiatelo molto)
Una volta che vi sentirete più a vostro agio con il software,
leggete lo "Pseudo" manuale dell'utente di Surfplan
e affrontare progetti più complessi come quelli di un foil,
di un bordo d'attacco, il profilo di un bordo di uscita, ecc.
Quindi progettate il vostro aquilone, fatelo (o fatelo fare da
qualcuno per voi), provatelo e inviateci foto e commenti per futuri lettori
della KitesurfingSchool.Org:
Uno dei migliori posti per apprendere come cucire un
aquilone gonfiabile è il sito web http://zeroprestige.org/ e
specialmente
http://web.media.mit.edu/~saul/iap2003/howto/howto.htm. Il
proprietario del sito fornisce una guida completa su tutte le fasi di
lavorazione per cucire il vostro aquilone personale dall'inizio alla
fine.
Se non siete abbastanza bravi per cucire il vostro aquilone,
potete chiedere a qualcuno di costruire il vostro aquilone su misura o
fornire uno dei vari progetti disponibili.
Unitevi a questi due gruppi, fate domande, usate il software,
cucite un aquilone (o trovate qualcuno che vi costruisca il vostro
aquilone su misura) e troverete che costruirsi un aquilone non è più
un'arte così misteriosa.
[se ci sarà abbastanza domanda, KitesurfingSchool.Org
proverà, in futuro, a scrivere una versione completa del manuale SurfPlan -
lasciatecelo sapere]
Surfplan, progettato e scritto da David Aberdeen, è un
software molto semplice da usare ma fintanto che non ha un manuale, il suo ricco
set di parametri può sopraffare il nuovo progettista di aquiloni (e anche un
disegnatore di foil). Finche Surfplan sarà il più usato per progettare gli
aquiloni LEI, in questo "Pseudo" Manuale dell'utilizzatore di Surfplan versione 4.5,
vi forniamo la descrizione di tutti i principali parametri per progettare un
aquilone con Surfplan (salteremo alcune parti dei foil come le briglie, ecc.).
La descrizione dei parametri è post anello stesso ordine in cui compaiono nel
menu EDIT di Surfplan:
This is one of the
most complex Surfplan's parameter menus you need to fill in so relax, read and
play around to understand the parameters properly before designing your own
kites:
Flat Wingspan:
The span of the kite in meters
Center Chord: The
center chord of the kite in meters
Calc size: Click
on this button to calculate the Wingspan and Center Chord using the total Surface
Area and Aspect Ratio (and the other already defined parameters). Most kite
designers would finalize these parameters at the end to have an "even" kite size or
aspect ratio number:
Flat Area: Total
surface area when flat or in other words, the size of the kite
Aspect Ratio:
Aspect Ratio of the kite (Wingspan * Wingspan)/Area. Most kite designers
would set this parameter from 4 to 7.
Tip Chord Ratio (%):
The length of the tip chord as a percentage of the center chord (less for more
stability, more for more depower, more radical control). Most designers
would set this parameter from 25% to 50% (if you set this number to 0 then you
are designing a 2 line LEI).
Num Cells/Panels
(Ribs in version 4.4 and older): Number of the kite panels.
Less for ease of sewing, more for smoother canopy (most
designers would set this parameter from 14 to 22 for LEI and 22 to 32+ for foils or Arcs
depending on the kite size).
Rib Spacing: How
and where to place the ribs (where the two panels are sewn together):
Equal Spacing:
Place the ribs at equal distance along the span of the kite (this is the default
option)
Proportional to Chord:
longer chord sections have ribs further apart.
Constant Area:
Place ribs such that each kite panel has the same area.
Manually Spacing:
Manually place the rib. Select this option and then click Edit Spacing to place the ribs manually.
Statistics: This
table shows all the current statistical information of the kite:
Flat Area
Flat Wingspan
Flat Aspect Ratio
Projected Area
Projected Wingspan
Project Aspect Ratio
Adjusted Area (Flat
Area/1.36). This number was "invented" by Bruno and used by many LEI kite
manufacturers as "kite size" in the past (mainly to compare a flat size LEI with
an average flat size foil - a 1.36 m2 flat size LEI is equal a 1 m2 average flat
size foil).
Leading Edge Length
Trailing Edge Length
Kite Shape:
Elliptical: Use
ellipse as the base shape of the kite (this is the default option and most
designers would select this option).
Percent Square:
0% for no effect (default), 100% for fully square or rectangle shape
Front Curvature:
0% for constant curving from center to tip (default), 100% for keeping the
center of the LE straight and curve more near the tip.
Rear Curvature:
similar to Front Curvature but for the Trailing Edge
Rectangular: The
kite has a rectangle shape
Triangular: Use
triangle as the base shape of the kite
Percent Square: 0% for
no effect, 100% for fully square or rectangle shape.
Scalloped TE:
Select if you want the trailing edge scalloped between 2 inflatable struts.
Amount (%): The
amount to scallop (in percentage of chord). The default is 1%. This is used
mainly to reduce the "flapping" of the trailing edge.
Curved LE: Not
used for LEI kite (this is mainly used for single skin kite to smoothly curve the LE
panels for the fibreglass rod).
Planar LE:
Make the Leading Edge of the kite stay in a 2 dimensional plane.
Manual Offsets: Select this to manually change the shape of the Leading and Trailing Edge of the
kite.
Edit LE: Edit the shape
of the LE
Edit TE: Edit the shape
of the TE
AoA Settings:
For some very good
discussion of the LEI's AoA and Profile Alignment Point settings, read
LEI Sphere Theory
Profile Alignment
Point (%): To change the forward/rearward sweep of the kite:
Center: The
amount to move the center of the kite forward (positive number) or rearward
(negative number) in percentage of the center chord. (most LEI kite designers
would set this from 20 to 40). The default value is 33%. For a 2
line LEI, Bruno has recommended that this alignment point should be around 42%
(with 0 degree built-in center AoA) for stability. Note that for Arc
kites, designers normally set this value closer to the leading edge than
Inflatable (Arc airfoil is a double skin with no turbulence at the front;
therefore the CoP of such airfoil is more forward than inflatable airfoil)
Tip: The amount
to move the tip of the kite forward or rearward in percentage of the wingtip chord.
(most kite designers would set this from 20 to 40 and similar to the Center
Profile Alignment Point). The default value is the same as Center Profile
Alignment Point at 33%.
AoA: The built-in
Angle of
Attack of the profiles:
Center: The
built-in AoA
of the center of the kite (most kite designers would set this from 0 to 5
degrees). The default value is 3 degrees.
Tip: The AoA of
the tip of the kite (most kite designers would set this from 0 to 5 degrees and
equal or more than the Center AoA).
The default value is 3 degrees.
AoA Rotation Point
(Chord %): The center point where the profile will rotate around when it
changes the AoA (in percentage of the chord). This value is dependent on the
profile and the value is normally from 20% to 40%. The default value is 33%.
It is best to use some other profile design and analysis tool to figure out this
value of the selected profile and enter it here.
In-Flight AoA
Analysis: This table shows the analysis of the AoA of the kite in-flight
(this table only shows the front line connection points at 0% and back line
connection points at 100% the chord of wingtips. For other connection
points, check the Sled Lines menu):
Vertical: At 90
degrees overhead:
Powered Down: The
AoA of the profile when the kite is fully depowered (no tension on
back lines).
CoP (Mid-power):
The AoA of the profile when the kite in mid-power (front lines and back lines
are equal). This value is calculated by Surfplan and normally the result is
close to the built-in AoA Center value specified in AoA Settings if the Profile
Alignment
Points are set close to the PAP of the Adjust AoA Analysis
Parameters menu (default at 33%).
Powered Up: The
AoA of the profile when the kite is fully powered up (no tension on front
lines). Most kite designer would make sure that this number is positive
and between 5 to 15 (larger number for more empower and possibility of reverse relaunch
if it is larger than the stall angle of the airfoil around 20 or higher).
At Window: At the
Wind Window overhead (normally at 85 degrees overhead):
Powered Down: The
AoA of the profile when the kite is fully depowered (no tension on
back lines).
CoP (Mid-power):
The AoA of the profile when the kite in mid-power (front lines and back lines
are equal). This value is calculated by Surfplan and the result is close
to the sum of the AoA Center value and the difference between 90 degrees and the
Wind Window degrees (specified in the Adjust AoA Analysis Parameters
menu) if the Profile Alignment
Points are set close to the PAP of the Adjust AoA Analysis
Parameters menu (default at 33%).
Powered Up: The
AoA of the profile when the kite is fully powered up (no tension on front
lines). Most kite designer would make sure that this number is positive
and between 5 to 20 (larger number for more empower and possibility of reverse relaunch
if it is larger than the stall angle of the airfoil around 25 or higher).
Effective Tow Point
(%): This show the effective tow point in percentage of chord when the
kite:
Powered Down: No
tension on back lines.
CoP (Mid-Power):
Front lines and back lines are equal. For LEI, Bruno has recommended that this
number should be around 42% for stability (actually, Bruno's recommendation is
for a 2 line LEI as one cannot change the effective tow point in that case).
Note that coincidently, the default values of Surfplan 4.5 will yield a value of
41.182 for this field. Note that for Arc, this value should be much
smaller (around 25% or so as Arc airfoil has little turbulence at the leading
edge thus the CoP is more forward).
Powered Up: No
tension on front lines.
Adjust AoA Analysis
Parameters: click this button to change the parameters used for the
In-flight AoA Analysis. It is best to use some profile design and analysis tool
to figure out these values for the center and wingtip profiles and enter them here (or
just use the default values):
CoP (%): Center
of Pressure of the kite in percentage of chord. Most designers would leave this
number at the default value of 33% (which is .33 due to a bug ???)
for LEI and 25% for Arc.
Wind Window:
The angle of the kite relative to the ground when it is stabilizing straight
overhead (most designers would leave this number at the default value of 85
degrees)
Straight: This is
the default value. The advantage of this option is that the designer can
have the flexibility of a batten wingtip, an appropriate profile wing tip or simply just
Dacron material (early 4 line LEI such as Naish AR5).
Elbow-joined: the
LE and the front of the wingtips are joined as an elbow. Most modern
designers would select this option.
Curved LE: The LE
is curved all the way to the back of the wingtip (there is no clear distinction
between the LE and the wingtip)
Scalloped:
The wing tip is scalloped.
Angled Wingtips:
Select this field and enter the angle of the wingtip (positive for
upward/rearward and negative for downward/forward)
Besides Size and Shape
menu, this is one of the more complex parameter menus in Surfplan. One
cannot design a profile with Surfplan but can import a profile and change some
parameters.
Profile Type:
Single Skin: for
single skin kites.
Double Skin: For foil or
Arc.
Inflatable: Select this
option for LEI.
Smooth Profiles: Surfplan will smooth out the profile
automatically if this option is selected (default is not
selected).
No Profile at Wingtip:
This is the default. Most modern designers would prefer some profile at wingtip.
LE Strut:
Segmented LE: This is
the default.
Armed LE: Using
the "Armed" method for making the LE strut.
Armed Limit: The number
of panels from the tip not to use the "Armed" method.
Center and Wingtips
Profile tables:
Profile Name: The name
of the profiles which have been loaded for the Center and the Wingtips
appropriately. The default profiles are DA2 for both Center and Wingtips.
Profile Depth: The
maximum depth (thickness) of the profile in percentage of chord (most designers would set
these values between 8% and 14%).
The default values are 9 for both Center and Wingtips.
At Chord (%): The
location of the maximum profile depth in percentage of chord. Most
designers would set this value between 18 and 33 depending on the profile.
The default values are 25 for both Center and Wingtip
Import: Click this
button to load an existing profile.
Export: Click this
button to save your profile for use in another kite designs.
Tube Size: The LE tube
size in percentage of chord. Surfplan will automatically calculate and
display the tube size in cm. Most designers would select tube size between 6%
and 12% of chord. The
default values are 9% for both Center and Wingtip tube sizes.
Seam Angle: Specify the
seam spot of the LE tube. The seam location is marked by a red marker. The default value is 45 degrees.
Sail Angle: Specify the
spot where the canopy is sewn onto the LE tube (marked by a red marker). The value has to be
between 0 and the Upper Limit (display next to the parameter) which is dependent
on the LE Tube Size. The default value is 45 degrees.
View Rib: Select
the rib to view its profile. The ribs are numbered from 1 at the Wingtip.
The ribs which have inflatable struts are marked with a "*" after the number.
Morph Profile:
Specify how the profile
along the wingspan will change from the Center profile to Wingtip profile. There is no need
to do anything here if the Center profile is identical to the Wingtip (even the
"No Profile at Wingtip" option is selected).
Auto: Morph from the
Center profile to Wingtip profile automatically (most designer would select this
default option):
By Distance/Chord:
Use this slider button to select how the morphing should be dependent on: by
distance and/or by chord. The default value is "By Chord" 100%.
Keep Center Profile (%
of Span): Use this slider to specify how far to retain the Center Profile from
the center of the kite. The default value is 0%.
Keep Tip Profile: Enter
the number of ribs from the wing tip to retain the wingtip profile.
Morphing Graph: A graph
in the table shows the result of the "morphing function" as specified by the
above parameters.
Manual: Select
this and click on the Change button to change the graph of the "morphing
function".
FEM Modelled Canopy (for
sled foils): Select this default option for LEI. If you are using some old
sample kite designs, make sure you select this option for Surfplan to update the canopy of
the old designs..
Manual Canopy (for
bridled foils): Select this if you design a bridle foil.
Detailed Canopy (for
bridled foils): Select this if you design a bridle foil (more manipulation than
the Manual Canopy option).
Certain kite material
will stretch on pressure. This menu provide a mean to specify how much
skin tension (how "stretchy") certain part of the kite may be exposed
to and therefore take
the anticipated stretch into account to compensate for the ultimate outcome.
Inflatable Strut
Tension: set the tension (stretch anticipation) on the LE and rib struts:
LE Factor: Set to 1 for
no tension and higher value for more tension and more stretch anticipation. Most
designers would set this to the default value of 1.2
Rib Factor: Most
designer would set this between 1 (no stretch anticipation, the default value) and 1.2 (same
pressure and tension as the LE).
Skin Tension: Most LEI
designer would leave this field at the default value of "None (Disable)"
This is another
important and complex Surfplan menu for LEI kites.
Use Ribs: Enter a
series of 0's and 1's (from Wingtip to Center) to specify where you want to have
inflatable struts (1's). The default is a string of "101010101" or 1
inflatable strut for every 2 ribs.
Rib Type: Select the
default value "Segmented Inflatable" for LEI kites.
Seams Underneath:
To specify the non-default location for seams (default is not selected) to have
a smoother canopy.
Irib Nose Shape:
To specify the nose shape of each individual inflatable strut (inflatable rib)
either round (0) or regular (1). Enter a string of 0's and 1's to
individually select the nose type of each strut from Wingtip to Center of the
kite. Select round nose strut (plumbing type of connection between the
struts and LE) for more rigidity and regular nose strut for
ease of sewing.
Round Tail Struts:
Select for round tails at the strut ends
Tail Angle: Enter the
tail angle of the ends of the struts (good for reducing drag and turbulence at
the strut ends).
Round-nose Struts:
Select to have all the struts with round-nose (plumbing type of connection between the
struts and LE). This makes the LE and strut connections more rigid and
more aerodynamic. This field has no effect if each strut's nose shape has been
defined in "Irib Nose Shape" field.
Upper LE Point
(degrees): Specify the upper location, in degrees, to connect the struts (Center
and Wingtip) to the LE. The default value for Center strut is 80 and for Wingtip
strut is 50.
Lower LE Point
(degrees): Specify the lower location, in degrees, to connect the struts
(Center and Wingtip) to the LE. The default value for Center strut is 0 and for
Wingtip strut is -30.
Center Diameter (%
Chord): Specify the maximum diameter of the strut in percentage of chord.
The default value is 7% for both center and wingtip strut. Most designers would set this value such that the
size of the strut is close (within 10% differences) to the size of the LE at that location.
TE Diameter (% Chord):
Specify the TE diameter of the strut in percentage of chord. The default
value is 2% for center strut and 5% for wingtip strut. Surfplan will calculate display the size in cm automatically.
Most designers would try to keep this value larger than 2.5cm or 3cm for practical
purposes (to be able to insert the bladder into the strut).
Number of Segments:
Specify the number of segments to use in the Center and Wingtip struts (default
5 for center and 3 for wingtip).
Seam Positions:
Specify the seam positions of the strut segments.
Automatic:
Calculate the seam position automatically using the Equal Angle/Equal Spacing
slider.
Manual: Calculate
the seam position semi-automatically using the Equal Angle/Equal Spacing slider
and the Seam Limit location specified in percentage of the length of the strut
(chord)
Reflex auto:
Similar to automatic; however, use the reflex profile algorithm
(for reflex profile)
Specify the lift
coefficients to compensate for the unequal lift characteristics between the
Center and the Wingtip profiles at the appropriate AoA(s). It is best to use some profile design and
analysis tool to figure out these values of the center and wingtip profiles and
enter them here (or just use the default values):
Center: Lift
coefficient for the Center profile (normally set to 1)
Tip: Lift
coefficient for the Wingtip profile relative to the Center (default value is 1,
the same as Center lift coefficient)
Flying Line Length:
Specify the line length in meters (the default is 30m; however, to save space,
the modern line length is 25m or even 20m).
Handle Separation:
Or bar length (the default value is 0.3m probably reflecting the fact that the
front lines are connected together while the back lines are normally .5m apart).
This is the same as
"Adjust AoA Analysis Parameters" in the Size and Shape menu. These
parameters are used for the In-flight AoA Analysis. It is best to use some
profile design and analysis tool to figure out these values for the center
profile and enter them here (or just use the default values):
CoP (%): Center of Pressure of the kite in percentage of
chord. Most designers would leave this
number at the default value of 33% (which is .33 due to a bug ???)
for LEI and 25% for Arc.
Wind Window: The angle of the kite relative to the ground
when it is stabilizing straight overhead (most designers would leave
this number at the default value of 85 degrees)
These are the seam
allowances for sewing purposes and normally default at 10mm for all the seams.
It's best to use the default values in the beginning and change them after you
have made 1 or 2 kites to suit your preferences.
Surfplan allows 4 line
connection points (6 if you count the default connection points at 0% and 100%
of Wingtip chord) on each Wingtip that can be used for either front lines or
back lines:
Line Attachment
Points: Specify the connection points in percentage of chord and click Apply
to view the updated In-flight AoA Analysis of these 4 connection points plus the
default at 0% and 100% of the Wingtip.
Mark Sled Line
Attachment Points: Select to have Surfplan marked the line attachment points
on the kite.
Uno degli ostacoli
per i nuovi progettisti di aquiloni è questa domanda "se cambio questo
parametro, cosa cambio?". Il vantaggio della teoria di Stelios e Timo
è che quando la capirete ed userete, tutti i parametri del programma Surplan
saranno intercorrelati e potranno essere facilmente messi in sintonia:
Aspect Ratio (AR)
Rapporto etremità dell'ala/corda centrale (Wingtip/Center
Chord Ratio)
Punto di allineamento del profilo (Profile Alignment Point
(PAP))
Angolo di attacco del centro dell'ala (Center AoA (at vertical))
Angolo di attacco dell'estremità dell'ala (Wingtip AoA (at
vertical))
Spessore del profilo centrale (Center Profile Thickness (in % della corda))
Spessore del profilo dell'estremità dell'ala (Wingtip Profile Thickness (in %
della corda))
dimensione del bordo di attacco (LE
tube size (in % della corda))
ecc.
Normalmente selezionate
lo
AR, il Rapporto etremità
dell'ala/corda centrale ed il PAP (circa il 42%
è richiesto dal brevetto di Bruno) dell'aquilone e poi calcolate tutto il resto
con la teoria della sfera. Cliccate qui per usare
la teoria della sfera che è basata su alcune
formule e indicazioni che Stelios ha inviato nella sezione Files del gruppo di
discussione InflatoDesign. Cliccate qui per i file .sle di Surfplan .sle
per un 4 lineeprogetto di aquilone LEI a 4 linee basato
sulla teoria della sfera. Alcune note sulla teoria della sfera:
Bruno attualmente ha
specificato 0° di AoA tipico (a riposo) nel suo diagramma. La corda
attraversa la base del tubo del bordo di attacco e la base del bordo di uscita.
Lo AoA della teoria della sfera originale può essere usato per calcolare la
dimensione del tubo. In Surfplan, la corda attraversa il centro del tubo
del bordo di attacco e la base del bordo di uscita. Per questo lo AoA
calcolato con Surfplan è 1/2 di quello della teoria della sfera originale.
Tutti i parametri
ottenuti potrebbero non essere in assoluto i migliori per i moderni aquiloni LEI;
comunque, sono ragionevoli e potranno funzionare.
Notate che la
teoria della sfera era basata su un aquilone LEI 2 linee con il PAP al 42% (Bruno
deve aver preso questo numero dalla "Hickhiker Guide to the Galaxy").
Questo progetto era necessario per un progettista nei giorni precedenti alla
possibilità dell'uso di CAD per il progetto di aquiloni che che potevano
essere bilanciati e guidati usando solo 2 linee attaccate all'estremità dell'ala
(2 linee e nessuna briglia - questo era il sogno dei minimalisti). Con un
moderno software di progetto di aquiloni a 4 linee LEI, il progettista e l'aquilonista
hanno molte possibilità di controllo, pertanto la "risposta dell'universo" 42
non sarà più necessaria. Quindi usate la teoria della sfera come guida per
progettare i vostri parametri. Siate avventurosi, con un aquilone LEI a 4 linee,
le possibilità sono senza limiti .....
nel messaggio
http://sports.groups.yahoo.com/group/kitesurf/message/17096 inviato al Kitesurf
Group, Bruno menziona che uno può progettare un aquilone LEI semplicemente
cambiando il parametro AR. Questo messaggio è stato il catalizzatore per
Stelios per sviluppare la teoria della sfera per il progetto di un aquilone LEI.
From: Bruno Legaignoux
<design@wipika.com>
Date: Thu Aug 3, 2000 2:44 am
Subject: Bruno Legaignoux's
message
Hi,
I'm Bruno Legaignoux. For
those which don't know my name, we are, with my brother Dominique the
inventors of the inflated kite in the shape of a gore. This message is to try to put
the numerous rumours off.
My brother and I were sailors
(French Junior champions, cruising boat skippers, sailing
instructors, surfers, windsurfers, etc...). We tried to develop very
efficient sails and boats and finally we became interested in kites when
seeing Jacob's Ladder, a catamaran pulled by Flexifoils, although we never
flied a dual line kite. It was in 1984. After a few researches, we
understood that no water relaunchable kite existed so it became obvious
to us that we had to create one. You can see some old photos
at www.wipika.com/Pages/chapitre1.html After one year of work, we
were sailing with water skis and demonstrating the device
during the 1985 Brest International Speed Week. We also applied for a
patent. The project was to find one or several licensees within 2
years but windsurfing was at its acme and no windsurf company was
interested.
We never stopped believing in
this sport so we had 10 years of VERY HARD time, continuing the project
without money, looking for new markets, for licensees, then creating our
own company and producing in France in 1993-94... at a too high cost
(please don't cry !)
Then Windsurfing declined and
Kiteboarding time came. I am proud to see that we
were the main actors of kiteboarding birth but for sure we were not
alone. For example Cory Roeseler with the Kiteski device or Andreas Kuhn with a
paraglider and a kind of wakeboard helped too with international media
exposure.
In 1995-96 we went in very
serious talks with Neil Pryde. Finally they renounced but they accepted to
produce small quantities for us and we started selling these kites
in July 1997 under Wipika brand mark. Then we found another
manufacturer in Asia.
In 1998, Don Montague and
Robby Naish came to us asking for a license. As it was our original goal,
we agreed and told them that both of us needed a software to be able to make
new designs quickly. I came to Hawaii and gave all my knowledge to Don
Montague and their programmers. One year later, the program was working. We
shared it. With it, everybody can make a new good kite in 30 seconds, just
changing one parameter. For example, change AR = 2.5 (the default value)
with 8 and you will appear as a genius designer!
WHY PATENT PROTECTION ?
Some people hate this way. I think that when you are a
well organized company in a market where products
evolve very quickly, patent
is just a waste of money and energy. But if you are a "small"
independent
inventor, you have no chance against large companies if you don't protect your
ideas : they won't even give you just credit for that !
Who on this list is against
intellectual property (music, literature, etc...) ?
Our motivation was kept
during the hard years because of the patent.
INFRINGERS
Seen by my side, there are
only 3 kinds of kites :
the ones which are far from
ours, like ram air kites, delta kites, etc...
the ones which are very
close to ours : if they got a license contract like Naish, they are licensees; if
not, they are infringing copies whether or not there are patented
improvements on.
there are kites designed
with a sole goal: to use our concept but escaping the patent by modifying the
kite after studying the patent and looking for weak points in it. In
this case it is more difficult for me to get the justice admitting the
infringement but I'll try each time I think I can win.
Obviously, I beat the
infringers and already stopped a few ones. Something interesting to be
known is that I have no obligation starting legal action immediately, that
means that I can start even when they will have invested a lot of energy
and money in their product. This is to explain that it is probably
more risky for them to infringe that what they generally think.
NEW LICENSEES SOON ?
Yes, we are open to give
other licenses but to companies which are able to bring something to
the market, not to companies with short term view or which sole way to get
market shares is to discount their kites. In 2000-2001 a few high image
companies will enter the market.
WHO INVENTED ?
- who invented kiteboarding ?
several people did it on their side without knowing that other
people previously made something close. Ourselves we started in 1984
with windsurf boards because we were surfers and windsurfers but
not waterskiers. We built several boards for that purpose. As our kites were very
unstable at that time, we mainly used waterskis because the
waterstart was easier, but the patent talks about windsurfing board type
too. We also tested any kind of
boats and many other "things" that you can't even imagine and a
patent drawing shows a guy on two 40cm "water skates" (photos in the
History page of www.wipika.com). We made and sailed them. It was fun. I 'm
sure that we'll soon see advanced pilots trying this kind of skates.
- who "invented" high AR
inflated kite ? In 1985 we made a 17m kite
with aspect ratio 6 and with 100% double-skin (photos on Wipika
web site... and a short video soon). With it, we waterskied with 6
to 12 knots of wind and, during the 1886 International Brest
Speed Week, we were clocked at 14.5 knots (average speed during a 500m
run) while the best world class windsurfers reached 10 knots.
This is registered. We also made kites with 20%,
30%, 40%, 60%, 80%, 100% double skin, what was already described in
the 1984 patent, and kites made of clear mylar with scrim.
Probably you will see this kind of "improvement" in the next
months or years.
- who "invented" inflated
"struts" without inner tube ? a competitor ? No, in the past, we used 2
different construction methods for inflated struts : airtight fabric and
mylar fabric with inner tube. These ways are described in
the original patent.
- who invented 4 line
straight bar with both front lines meeting at a "main line" going to the
harness and with the bar sliding along the "main line" ? a competitor ?
No, we own a patent on this device since 1995. I first used this device for
buggying and won some races thanks to it. Seasmik uses without any
license the exact device we described so we'll have to sue them.
- who invented 4 line
inflated kite ? A competitor ? No, the above patent also describes how to
settle inflated kites with 4 lines by cutting the edges for example
(there are other ways). I always used "cut tip" kites with the 4
line straight bar. I explained all these things
to Don Montague in 1998. Why didn't we apply these
improvements earlier ? There are 2 main reasons :
Firstly, when you settle a
company and you have no money, especially in France, you have to work 80
hours a week to have it working properly. So I had no time for R&D.
It's why in 1999 I looked for people to take care of Wipika and get myself
more time in R&D. I also moved in early 2000 to Dominican Republic
which is really a perfect place for R&D.
Secondly, the market was not
ready for more evolved kites. In the "early ages", we made very
efficient kites then we understood that we had to make simple, stable
and safe. In 1998, 100% of the users
were beginners - there are not so many markets like this one ! In 1999, still 90% were
beginners but the 10 other percents were starting to ask for more
efficient kites so we prepared the Free Air AR3.3 range and started sales
in early 2000. But because of Naish AR5 our new range is already old
fashioned if you believe a few ones. My main concern is safety and
when I hear that some beginners directly purchase AR5 kites, I'm
scared. Firstly they are more difficult to relaunch but above all they
are fast. That makes them dangerous for beginners in the state of the
market (almost no schools nor well informed retailers...).
We are starting a competition
to efficiency, just like windsurfing manufacturers did. Remember : "Hey guy, how many cambers do
you have ? Only six ? ... and your board, what size ? 2.26m
? Too bad! mine is 2,195m !". Windsurfing is dying for this
reason. And us, when ? A fact : the Wipika riders
Franz Olry and Christopher Tasti, which actually win some
events, don't want to use too high AR kites because they are so fast and
unstable that they can't make the kind of tricks they do with more
stable kites. They don't want a 20 kite quiver. They want simplicity.
Same for Lou Wainman, Mauricio Abreu and some other ones. If you see them using high AR
kites, it's because competition pushes in this way, not because they
prefer (except in light winds). To resume, if we go too
quickly, we'll burn our wings. All the people involved in kiteboarding
should take care with that.
R&D AGREEMENT WITH NAISH ?
Any kind of commercial/strategical
agreement was never made. Both companies are completely independent/free of mutual contract. Both are Legaignoux licensees
with same contract terms.
4 LINE KITES
Wipika supplies the Classic
kites since July 1997 with an additional webbing so that all the
Classic can be settled with 4 lines. That means that we believe to the
4 line use since a long while but 99% of the customers didn't want
to hear about it last year. There are several ways to
settle your Classic as a 4 line kite, I'll come back on this matter
in another message. Very soon, the Classic kites
will be sold with a second webbing, like the Free Air, to simplify
transformation. Classic and Free Air will
also receive long velcros to fold the tips. Many new Wipika items will be
available in the next weeks and months, including an
interesting 4 line bar. We'll keep you informed. You are welcome to use
abstracts of this message for public use as long as it is in good faith. Please don't expect that I'll
react to the messages which could follow mine, I'm still too busy to
do it. Sorry!
[When Peter released
these myths, it created many controversial debates and one of the reasons was
that it's not clear what Peter meant by "angle of attack". Note that Peter
talked about kite design here so the "angle of attack" he referred to
probably meant "built-in AoA" and not the AoA of the kite when flying]
From:
"Ian Young" <IanYoung@iinet.net.au> Date: Thu Aug 3, 2000
7:34 pm Subject: Peter Lynn's Six
Aerodynamic Myths of Kite Traction I
Food for thought from Peter Lynn for those of you who don't
get his
newsletter ...
The Six Aerodynamic Myths of Kite Traction.
Myth One.
That the upwind performance (that is, lift/drag ratio) of kites is
primarily
a function of profile and aspect ratio.
Wrong. The strongest determinant of L/D is angle of attack. Low
angles of
attack yield high L/D in an inverse relationship, profile and
aspect ratio
have comparatively little effect.
Myth Two.
That the Lift Coefficient (power for size) of a kite is primarily
determined
by it's profile and aspect ratio.
Wrong. Angle of attack is again by far the strongest determinant
of pull
for area, and by close to a direct linear relationship in the
range that
matters for kites.
Myth Three.
That high aspect ratio equates to high performance.
Correct in theory but misleading for kites in practice. Aspect
ratio
(defined as span squared divided by area) is a strong determinant
of induced
drag, the dominant form of drag at low speeds for efficient
airfoils- but
kites are not efficient airfoils by any definition, so aspect
ratio
determined induced drag is not the major drag component for kites.
It would
be possible to make a square wing (A.R=1.0) that is more efficient
than the
highest aspect ratio high performance kite currently available-
(but making
it useable as a kite would be another matter).
Myth Four
That Thin sections are "better" than fat sections.
Wrong. Unless your kite is to fly at something approaching the
speed of
sound anyway. Sections as fat as 16% (maximum thickness as a
proportion of
chord) lose nothing by L/D or lift coeff. to thinner sections up
to 300km/hr
or so and are less prone to stalling and luffing.
Myth Five.
That double skin wings (ie three dimensional airfoils) are more
powerful
than cambered single skin wings.
Wrong. Cambered single skin wings will generally have higher lift
coefficients than fully shaped 3 dimensional wings because they
can work at
higher angles of attack without stalling. 3 D forms will be more
luff
resistant and can have higher L/D but they won't be more powerful.
Tanstafl. (There ain't no such thing as a free lunch.)
The fundamental design conflict is between one and two above.
Traction
kites require high angle of attack to have desirable power for
size
characteristics but low angle of attack for good upwind
performance.
Some kitesurfing tips:
*Early this year we added an extra valve near the wingtips on Arcs
to speed
their inflation and to make them more resistant to tip collapse in
the case
that inflation leaks develop. We aren't sure that this was
necessary but
added them just in case. Being near the tips, the disadvantage of
these
extra valves is that they can ingest water during relaunching. If
this is
a problem for you just seal them off internally with double sided
tape- they
can then easily be reopened if ever necessary. Thank you to Nick
Grant for
this.
*If you're going to break things, it is not a good idea to do so
when
against wind and tide and far from land. In Tahiti last week Mike
Holland
broke a line in such circumstances and was unable to re-rig, and
relaunch so
spent one day of his South Pacific holiday swimming in. Thank you
Mike for
this tip.
*When you are using our wrist leash velcro'd to the bar end so
that it
doesn't get twisted up in spins, lash it on with knitting wool in
addition
to the velcro so that it doesn't come off prematurely but will
still release
when required- just like wool ties on a yacht spinnaker. Thank the
sheep
for this one.
New things this month- Nothing!, Which is the first time ever,
except that
there is something but I'm just not talking about it until we hear
back from
our travelling testers. It was what Mike was testing in Tahiti
when he had
a line break and the long swim.
And a little gossip to round off: Andy Reid; windsurfer,
kitesurfer,
boardmaker and (with Justin), our kite test rig operator, finishes
his B
Eng. this year and goes to work at Team New Zealand for the next
defence of
the America's Cup. Our loss, their gain- congratulations Andy.
Peter Lynn, Ashburton New Zealand, July 31, 2000.
Cheers,
Ian Young
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