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technologie et réglementation technique - iate.europa.eu
Base drag reduction caused by riblets on a gaw(2) airfoil... • - base pressure coefficient, (pb- pjlgx airfoil chord riblet height • = local static pressure • = freestream static pressure • = freestream dynamic pressure = trailing-edge thickness friction velocity = distance along...
général - core.ac.uk - PDF: nal-ir.nal.res.in
Wind tunnel investigation of control surface characteristics. 12 - various cover-plate alinements on the naca 0015 airfoil with a 30 percent chord flap and large sealed internal balance /... The chord of the straight-contour flap was 30 percent of the airfoil chord and the balance with 50 percent of the flap chord.Prepared...
Design procedure for low-drag subsonic airfoilsAirfoil has least amount of drag under given restrictions of boundary layer transition position, lift coefficient, thickness ratio, and Reynolds number based on airfoil chord....
Natural-laminar-flow airfoil development for a lightweight business jet... Nomenclature Cd = section pro le drag coef cient Cl = section lift coef cient Clmax = section maximum lift coef cient Cm = section pitchingmoment coef cient about quarter-chord point C p = pressure coef cient C p;sonic = critical pressure coef cient c = airfoil chord, m M = Mach number MDD = drag-divergenceMach number,Mach number at which d.Cd/=dM...
Wind-tunnel investigation of the boundary layer on an naca 0009 airfoil having 0.25- and 0.50-airfoil chord plain sealed flaps /...0.50-airfoil chord plain sealed flaps....
technologie et réglementation technique - iate.europa.eu
Effect of leading edge protuberance on thrust production of a dynamically pitching aerofoil... They are characterized by an amplitude and wavelength of 12% and 50% of the aerofoil chord length respectively....
général - core.ac.uk - PDF: eprints.gla.ac.uk
Numerical investigation on flow separation control of low reynolds number sinusoidal aerofoils...14,000.The protuberances are characterized by an amplitude and wavelength of 12% and 50%of the aerofoil chord length respectively....
Effects of gurney flap on supercritical and natural laminar flow transonic aerofoil performance...0.7% aerofoil chord length....
 PDF: core.ac.uk
The pressure drag of an aerofoil with six different round leading edges, at... Notation cD cL 0 pressure drag coefficient lift coefficient aerofoil chord length H total pressur
The influence of hole orientation on the aerodynamics of battle damaged wings... To represent different attack directions, the inclination of the hole axis relative to the aerofoil chord was varied....
 PDF: core.ac.uk

Synonymes et termes associés français

Exemples français - anglais

transports aérien et spatial / sciences naturelles et appliquées / transport terrestre / transports - iate.europa.eu
transports aérien et spatial - iate.europa.eu
sciences naturelles et appliquées / transport terrestre / transports - iate.europa.eu
transports aérien et spatial - iate.europa.eu
transports aérien et spatial - iate.europa.eu
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Traductions en contexte français - anglais

Le profil aérodynamique comprend des parois latérales de pression et d'aspiration définissant des bords avant et arrière espacés l'un de l'autre dans le sens de la corde du profil aérodynamique.

The airfoil includes pressure and suction sidewalls defining chordally spaced apart leading and trailing edges of the airfoil.

industrie mécanique - wipo.int
La première aile et/ou la seconde aile s'étend sur au moins environ 35 % de la corde du profil aérodynamique de pale.

At least one of the first wing and the second wing extends at least about 35% of the chord of the airfoil.

industrie mécanique - wipo.int


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