correction menu français

[gs102]

dans 101,102,103 j'avais un doute sur les cordes d'embase etc.. il s'agit en fait de corde d'emplenture (base), corde de saumon (extremité) et a d=25% du bord d'attaque a l'emplanture la corde aerodynamique moyenne (ou cam), non?

[letibo1]

Salut Georges et Beber, pour les termes techniques pur aviation, je ne pourrais t'aider. Mais je vais me renseigner.

Voilà encore et encore la suite



44 -all propellers|auto-feather after engine failure { Some twins have auto-feathering props. In this case, the prop will automatically feather to reduce drag after an engine failure. It would be certain death in a helicopter, as the rotor would automatically feather to produce no lift after an engine failure!

45 tous moteurs|throttle-by-wire and automatic mixture { Some engines, such as the Corvette LS-1 and LS-6 used in some homebuilts, have drive-by wire throttles to maintain their RPM more precisely and keep the optimum fuel-air mixture, despite varying engine loads and air densities. Check that here.

322 feathered pitch of prop|(deg) { This is the pitch of the prop when feathered, if it is a featherable prop.

46 reverse pitch of prop|(deg) { This is the pitch of the prop when in reverse, if it is reverse-equipped in the other engine screen. Be sure to enter a negative number if the pitch is negative, as it probably is!

47 prop mass ratio|(compared to solid aluminum) { This is how heavy the prop or rotor is compared to one made of pure aluminum. Composite props, for example, are lighter. Heavier props speed up and slow down more slowly, and provide more auto-rotation ability in helicopters.

48 tip weights on ROTORS|(pounds, each) { This is how many pounds of weight are in EACH rotor tip, increasing the rotor inertia, which is useful for helos and autogyros.

49 tip mach at 100% power|(for constant-mach props) { If you selected a constant-mach prop as the prop type, then the prop governor will automatically adjust the prop pitch to speed or slow the prop to try to maintain this mach number at the prop tip at 100% power (interpolating across the throttle range of travel).

50 tip mach at 50% power|(for constant-mach props) { If you selected a constant-mach prop as the prop type, then the prop governor will automatically adjust the prop pitch to speed or slow the prop to try to maintain this mach number at the prop tip at 50% power (interpolating across the throttle range of travel).

53 puissance maxi|(hp) { This is the maximum horsepower output of the engine, obtained at sea level at standard temperature and density.

576 transmission perdue|(part) { This is how much of the engine's power is lost to the transmission. You should have about 0.00 to 0.02 for regular airplanes, 0.04 for single-engine helos, and 0.06 for twin-engine helos. This should include all drags on the engine, including any generators, belts, chain-drives, etc. that detract from the full rated power.

55 altitude critique|(feet) { Engines generally put out less power at high altitude due to thinner air, but turbocharging can keep packing in air even at high altitudes. The critical altitude is the highest altitude at which the engine can still put out FULL POWER. This altitude can be above sea-level either by putting a turbocharger on a reciprocating engine or down-rating a jet or turboprop. Enter 0 for the critical altitude here if you are doing neither. :arrow:

[gs102]

Salut les traducteurs! c'etait deja fait mais ca a du se perdre dans les mails... a plus

44 -all propellers|auto-feather after engine failure { Some twins have auto-feathering props. In this case, the prop will automatically feather to reduce drag after an engine failure. It would be certain death in a helicopter, as the rotor would automatically feather to produce no lift after an engine failure!

44 toutes hélices peuvent avoir une fonction de pas auto-débrayable en cas de panne moteur (certains bi-moteurs on des helices autodébrayables, dans ce cas l'hélice débraye pour réduire la trainée apres l'arrêt du moteur. C'est la mort assurée sur hélico, si l'hélice debraye et ne produit plus de sustentation après la panne moteur!

88 tous les moteurs|inversion disponible { La poussee peut etre inversée.

45 tous moteurs|throttle-by-wire and automatic mixture { Some engines, such as the Corvette LS-1 and LS-6 used in some homebuilts, have drive-by wire throttles to maintain their RPM more precisely and keep the optimum fuel-air mixture, despite varying engine loads and air densities. Check that here.

45 tous moteurs peuvent disposer de la gestion des gaz et mixture assistée ( Certains moteurs comme le Corvette LS-1 et LS-6 utilisés dans certaine constructions maison ont un système de gestion des gaz pour maintenir leur régime plus précisément et maintenir un mélange air /carburant optimaux en dépit des charges moteur ou des différentes densités de l'air.

322 feathered pitch of prop|(deg) { This is the pitch of the prop when feathered, if it is a featherable prop.

322 pas d'helice debrayée (deg) (ceci est l'angle de l'hélice quand elle est débrayée, s'il s'agit d'une helice débrayable.

46 reverse pitch of prop|(deg) { This is the pitch of the prop when in reverse, if it is reverse-equipped in the other engine screen. Be sure to enter a negative number if the pitch is negative, as it probably is!

46 angle d'inversion du couple de l'hélice (deg) (Ceci est l'angle d'incidence de l'hélice quand son couple s'inverse si équipée de l'option inversion de couple dans l'autre écran moteur.Assurez vous d'entrer une valeur négative si le couple est négatif comme c'est probablement le cas!

47 prop mass ratio|(compared to solid aluminum) { This is how heavy the prop or rotor is compared to one made of pure aluminum. Composite props, for example, are lighter. Heavier props speed up and slow down more slowly, and provide more auto-rotation ability in hélicopters.

47 Coefficient de masse de l'hélice (comparée a celle de l'aluminium pur) (ceci definit le poids de l'helice ou rotor par rapport a sa réalisation alu. Les hélices en composite sont plus legeres. Les helices plus lourdes accelerent et ralentissent plus lentement et provoquent un meilleur contrôle de l'autorotation en hélico)

48 tip weights on ROTORS|(pounds, each) { This is how many pounds of weight are in EACH rotor tip, increasing the rotor inertia, which is useful for helos and autogyros.

48 masses d'extremités de voilure sur rotors (livres, chaque une) (ceci est le poids en livres de Chaque masse d'extremite de chaque pale du rotor augmentant l'inetie ce qui est utile pour les helicos et autogyros.

49 tip mach at 100% power|(for constant-mach props) { If you selected a constant-mach prop as the prop type, then the prop governor will automatically adjust the prop pitch to speed or slow the prop to try to maintain this mach number at the prop tip at 100% power (interpolating across the throttle range of travel).

49 vitesse en mach de l'extremité des pales a 100% de la puissance (pour helices a mach constants) (Si vous avez sélectionné une hélice a mach constant.Le gestionnaire d'helice va automatiquement ajuster le couple de l'helice pour ralentir ou accélerer la rotation vers ce nombre de mach a l'extremité des pales a100% de la puiissance (interpolation avec la course de la commande de gaz)

50 tip mach at 50% power|(for constant-mach props) { If you selected a constant-mach prop as the prop type, then the prop governor will automatically adjust the prop pitch to speed or slow the prop to try to maintain this mach number at the prop tip at 50% power (interpolating across the throttle range of travel).

50 vitesse en mach de l'extremité des pales a 50% de la puissance (pour helices a mach constants) (Si vous avez selectionné une helice a mach constant.Le gestionnaire d'helice va automatiquement ajuster le couple de l'helice pour ralentir ou accelerer la rotation vers ce nombre de mach a l'extremité des pales a 50% de la puiissance (interpolation avec la course de la commande de gaz)

53 puissance maxi|(hp) { This is the maximum horsepower output of the engine, obtained at sea level at standard temperature and density.

53 Puissance Maxi (CV) (Ceci est la puissance max en CV produite par le moteur, obtenu au niveau de la mer et temp et dens standard

576 transmission perdue|(part) { This is how much of the engine's power is lost to the transmission. You should have about 0.00 to 0.02 for regular airplanes, 0.04 for single-engine helos, and 0.06 for twin-engine helos. This should include all drags on the engine, including any generators, belts, chain-drives, etc. that detract from the full rated power.

576 transmission, pertes|(Ceci est l'énegie moteur perdue dans la transmission.Vous devriez avoir 0,00 a0,02 pour les avions courants, 0,04 pour les hélicos a moteur unique, et 0,06 pour les helicos bi-moteurs. Ceci doit inclure toutes les charges moteur comme les generateurs, courroies, transmissions par chaîne etc... qui prélèvent de l'énergie sur la puissance nominale

55 altitude critique|(feet) { Engines generally put out less power at high altitude due to thinner air, but turbocharging can keep packing in air even at high altitudes. The critical altitude is the highest altitude at which the engine can still put out FULL POWER. This altitude can be above sea-level either by putting a turbocharger on a reciprocating engine or down-rating a jet or turboprop. Enter 0 for the critical altitude here if you are doing neither.

55 altitude critique (pieds) (Les moteurs délivrent généralement moins d'énergie a des altitudes élevées due a la raréfaction de l'atmosphère, mais le turbocompresseur remèdie a cela même aux altitudes élevées. L'altitude critique est l'altitude a laquelle le moteur peut encore delivrer sa pleine puissance. Cette altitude peut etre au dessus du niveau de la mer en ajoutant un turbo compresseur a un moteur a pistons ou en diminuant la capacite d'un jet ou turbo prop. Entrez 0 si vous ne voulez rien

[Daniel_L]

auto-feather n'est pas auto-débrayable mais mise en drapeau automatique.

Daniel

[gs102]

Oui la dessus j'ai un peu "improvisé mais je me comprends" mais pour les autres ca sonne effectivement beaucoup plus juste lol... Pendant que j'y suis...que penses -tu des 101,102 et suiv (4 ou5 posts en arriere concernant les cordes d'emplenture de saumon et a 25%....) je pense qu'il faut etre prècis sur le sujet si on veut des avions qui volent bien!
Merci Daniel!... elle va etre au top notre traduc!

[letibo1]

Ok Daniel, j'en ai pris note, et réadapté le texte.

Effectivement Georges, je n'ai pas eu la traduction de la ligne 44 à 55. Maintenant c'est ok, merci.

Jai une bonne nouvelle, on a dépassé la moitié, c'est dire la richesse de Plane-Maker.

J'aimerais savoir s'il y a un synonyme à "Emplenture".

sinon voici la suite, et j'espère que d'autres personnes contribueront à cette traduction.

146 -toutes helices|beta-range available { beta is neither forward nor reverse thrust. It is simply putting the prop at zero degrees pitch, throttle at idle. Doing this provides some drag without working the engine. Certains bi-moteurs en sont equipes. Cochez ici si votre appareil a ce systeme.

118 -rudder 1 { This indicates whether this part (element) of the vertical stabilizer is equipped with rudder pedals. Rudders are used to yaw the aircraft in flight. The rudders are linked (possibly via a fly-by-wire system) to the rudder pedals.


111 -flap 1 { This indicates whether this part (element) of the wing is equipped with flap-set 1, which increase the amount of lift (and, incidentally, drag) that the wing produces when the flaps are deployed (which is accomplished with a large white handle in the cockpit).


112 -slat { This indicates whether this part (element) of the wing is equipped with slats, which allow the wing to get to a higher angle of attack before it stalls.

116 -aerofreins { This indicates whether this part (element) of the wing is equipped with speedbrakes, which can be deployed by a small white handle in the cockpit to reduce lift and increase drag, thus speeding descent
.
335 -incidence with ail1 { This indicates whether this part (element) of the wing changes incidence with aileron input.


142 -incidence with elevator 1 { This indicates whether this part (element) of the wing changes incidence with elevator input.


143 -incidence with rudder 1 { This indicates whether this part (element) of the wing changes incidence with rudder input.


336 -incidence with vector { This indicates whether this part (element) of the wing changes incidence with thrust vector.

296 -incidence with trim { This indicates whether this part (element) of the wing changes incidence with trim (like for flying stabilizers on airliners and Mooneys).

309 MODE EDITION
310 RESET THIS SECTION TO VERTICAL
311 RESET ALL SECTIONS TO VERTICAL
312 LOAD TOP BACKGROUND BITMAP
333 CLEAR TOP BACKGROUND BITMAP
313 LOAD LEFT BACKGROUND BITMAP
334 CLEAR LEFT BACKGROUND BITMAP

300 RESET EDITING OFFSETS (arrows and +/- to change)
299 SWITCH EDITING MODES

124 body radius|(ft) { This is simply the width in feet of the grids below, which you should set to be just big enough to draw all the cross-sections of the aircraft.

125 body coeff of drag|(based on BODY FRONTAL AREA) { This is the coefficient of drag for this body, which will give the total drag for the body when multiplied by the body frontal area, air density squared, airspeed squared, and then divided by 2. A value of 0.1 is appropriate for airplanes of average sleekness. 0.05 would apply to very low-drag aircraft.

120 |-aircraft has fuselage (might be no for flying wings) { The fuselages and other bodies in X-Plane contribute drag, and even some lift and sideforce, based on their frontal, side, and top areas. They also change the moments of inertia of the craft by distributing the aircraft's mass across the surface of the fuselage, wings, stabilizers, and other bodies. Like every part on the plane in X-Plane, they have aerodynamic as well as visual consequences.

123 |-aircraft has this external fuel tank, float, or other external body

121 |-aircraft has a nacelle over this engine { The fuselages and other bodies in X-Plane contribute drag, and even some lift and sideforce, based on their frontal, side, and top areas. They also change the moments of inertia of the craft by distributing the aircraft's mass across the surface of the fuselage, wings, stabilizers, and other bodies. Like every part on the plane in X-Plane, they have aerodynamic as well as visual consequences.

532 long arm|(ft) { fuel tank, float, or other external body
533 lat arm|(ft) { fuel tank, float, or other external body
534 vert arm|(ft) { fuel tank, float, or other external body

535 { this fuselage cross section

[gs102]

Oui! je fais une petite pause... au suivant!
(Tres instructif comme travail... on y prend gout....)
De corde en aiguille j'ai trouvé l'emplanture ici:
http://epervier.sudluberon.free.fr/spp/12cam.htm
a plus
jojo

[letibo1]

Excellent, et tres intructif.

[milan]

pour des question de traduction, ce site pourrait peut-être t'aider
le site en question

[gs102]

Peut être aider?... en plein dans le mille(an) oui! ...(bof, excuses...)
juste ce qui nous manquait!
merci

[milan]

Pour de l'anglais (et autres) moins tchnique, voici un site très riche pour la traduction
WordReference

[Daniel_L]

Dans la série des dictionnaires utiles, j'aime beaucoup celui-ci :

http://www.granddictionnaire.com/btml/fra/r_motclef/index1024_1.asp

Le Grand dictionnaire Terminologique est un site du Québec qui propose des traductions par domaines. "Rudder" par exemple peut être traduit par "gouverne de direction" en aéronautique et par "gouvernail" en marine.

Daniel

[Caravelle]

Dans la série aussi, j'aime bien Lexilogos :

http://www.lexilogos.com/francais_langu ... naires.htm
qui regroupe pleins de dictionnaires différents.

et pour les traductions, j'aime beaucoup Altavista :
http://babelfish.altavista.com/translate.dyn

Mais on digresse là

[letibo1]

Mouais, je préfère le site de Milan sur le coin des passionnés...vraimant bien fait.

Pour le reste, j'ai vraimant besoin des traductions......et voici la suite....A VOS CLAVIERS:


126 aileron 1 chord ratio| { Ailerons are mounted on the wingtips and move in opposite directions to ROLL the airplane. The chord ratio is the fraction of the wing, from leading edge to trailing edge, that the control surface takes up. Controls typically have a chord ratio of about 0.2 to 0.3. Two sets of ailerons are provided so you can have inboard and outboard ailerons with different deflections. THIS IS THE CHORD RATIO AT THE ROOT THEN TIP OF THE CONTROL.



128 elevator 1 chord ratio| { Elevators are mounted on the horizontal stabilizer (tail) of the airplane and move to PITCH the airplane. The chord ratio is the fraction of the wing, from leading edge to trailing edge, that the control surface takes up. Controls typically have a chord ratio of about 0.2 to 0.3. THIS IS THE CHORD RATIO AT THE ROOT THEN TIP OF THE CONTROL.



129 rudder 1 chord ratio| { Rudders are mounted on the vertical stabilizer (tail) of the airplane and move to YAW the airplane. The chord ratio is the fraction of the wing, from leading edge to trailing edge, that the control surface takes up. Controls typically have a chord ratio of about 0.2 to 0.3. THIS IS THE CHORD RATIO AT THE ROOT THEN TIP OF THE CONTROL.


130 spoiler 1 chord ratio| { Spoilers are mounted on the wingtips and move one at a time to ROLL the airplane. The chord ratio is the fraction of the wing, from leading edge to trailing edge, that the control surface takes up. Controls typically have a chord ratio of about 0.2 to 0.3. THIS IS THE CHORD RATIO AT THE ROOT THEN TIP OF THE CONTROL.

131 drag rudder chord ratio| { Drag rudders are mounted on the wingtips of flying wings and open up to create drag to YAW the airplane. The chord ratio is the fraction of the wing, from leading edge to trailing edge, that the control surface takes up. Controls typically have a chord ratio of about 0.2 to 0.3. THIS IS THE CHORD RATIO AT THE ROOT THEN TIP OF THE CONTROL.

132 speedbrake chord ratio| { Speedbrakes are mounted anywhere on the wing and open up to increase drag and decrease lift to slow the airplane. The chord ratio is the fraction of the wing, from leading edge to trailing edge, that the control surface takes up. Controls typically have a chord ratio of about 0.2 to 0.3. THIS IS THE CHORD RATIO AT THE ROOT THEN TIP OF THE CONTROL.

137 |control surface up/down { Ailerons are mounted on the wingtips and move in opposite directions to ROLL the airplane. They might move 20 degrees typically.

139 |aircraft nose up/down { Elevators are mounted on the horizontal stabilizer (tail) of the airplane and move to PITCH the airplane. They might move 20 degrees typically.

133 |rudder left/right { Rudders are mounted on the vertical stabilizer (tail) of the airplane and move to YAW the airplane. They might move 30 degrees typically.

134 |spoiler up { Spoilers are mounted on the wingtips and move one at a time to ROLL the airplane. They might move 30 degrees typically.

135 |drag rudder def { Drag rudders are mounted on the wingtips of flying wings and open up to create drag to YAW the airplane. They might open 45 degrees typically.

136 |speedbrake def { Speedbrakes are mounted anywhere on the wing and open up to increase drag and decrease lift to slow the airplane. They might open 30 degrees in flight typically.

140 stab trim, NOSE up then down { This is how many degrees the entire stabilizer can move up or down for trim control. Most airplanes can NOT move the entire stabilizer for trim control, and they should have ZERO here. Airliners are the exception, which must move their entire stabilizer to trim the aircraft.

141 |(degrees, if you want the stabilizer to move in trim) { This is how many degrees the entire stabilizer can move up or down for trim control. Most airplanes can NOT move the entire stabilizer for trim control, and they should have ZERO here. Airliners are the exception, which must move their entire stabilizer to trim the aircraft.

144 corrugated with gaps-smooth with gaps-smooth with no gaps-high energy slots

148 control surface type { This will impact how effective the control surfaces are in X-Plane.

145 plain flap-slotted flap-slotted fowler-double slotted fowler-triple slotted fowler-split flap
303 krueger flap-slat

304 slat type { This will control how much angle of attack gain you get before stalling in X-Plane.

149 flap 1 { This will control how much lift, drag, and moment the flaps produce in X-Plane.

[letibo1]

C'est quand même dommage de s'arreter en si bon chemin :?: