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portance maxima

maximum lift

transports aérien et spatial - iate.europa.eu

Moment de portance maximal (par rapport à l'axe de rotation)

Maximum lift moment (relative to the axis of rotation)

général - CCMatrix (Wikipedia + CommonCrawl)

Un décrochage est une perte de portance et une augmentation de traînée qui se produit lorsque l'aéronef vole à un angle d'attaque supérieur à l'angle qui assure la portance maximale.

A stall is a loss of lift and an increase in drag that occurs when an aircraft is flying at an angle of attack greater than the angle that provides maximum lift.

général - CCMatrix (Wikipedia + CommonCrawl)

Un décrochage est une perte de portance et une augmentation de traînée qui se produit lorsque l'aéronef vole à un angle d'attaque supérieur à l'angle qui assure la portance maximale.

A stall is a loss of lift and increase in drag that occurs when an aircraft is flown at an angle of attack greater than the angle for maximum lift.

général - CCMatrix (Wikipedia + CommonCrawl)

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Effects of mach number up to 0.34 and reynolds number up to 8,000,000 on the maximum lift coefficient of a wing of naca 66-series airfoil sections /...0.34 and Reynolds number up to 8,000,000 on the maximum lift coefficient of the wing of NACA 66-weries airfoil sections are presented....

général - core.ac.uk - PDF: www.hathitrust.org

Maximum lift/drag ratio of flat plates with bluntness and skin friction at hypersonic speedsNewtonian theory is used to derive a simple expression for the maximum lift/drag ratio of flat plates with bluntness and skin friction at hypersonic speeds....

PDF: hdl.handle.net

An investigation of blowing as a method of increasing the maximum lift of a double-wedge airfoilThis report presents the results of an investigation of boundary layer energization by blowing as a method of increasing the maximum lift coefficient for supersonic airfoils operating at low subsonic speeds.The...

PDF: thesis.library.caltech.edu

Factors affecting the maximum lift-drag ratio at high supersonic speeds /A study of the factors affecting the maximum lift-drag ratio has been conducted in an effort to determine how to obtain high aerodynamic values at high supersonic Mach numbers.NACA...

PDF: www.hathitrust.org

Preliminary investigation of the effect of compressibility on the maximum lift coefficient, special reportPreliminary data are presented on the variation of the maximum lift coefficient with Mach number....

PDF: hdl.handle.net