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upper surface camber

См. также в других словарях:

  • upper camber — The curvature of the upper surface of an airfoil. It is the distance between the mean camber line and the chord line when the mean camber line lies above the chord line. Also called a positive camber. See also camber …   Aviation dictionary

  • camber — i. The curvature of an airfoil above and below the chord line surface. It is the distance between the mean camber line and the chord line. Where the mean camber line lies above the chord line, the airfoil is said to have a positive camber.… …   Aviation dictionary

  • camber — /ˈkæmbə / (say kambuh) verb (i) 1. to arch slightly; bend or curve upwards in the middle. –verb (t) 2. to cause to arch slightly. –noun 3. a slight arching or convexity above, as of a ship s deck or a road surface. 4. a slightly arching piece of… …  

  • negative camber — i. An airfoil in which the mean camber line lies below the chord line. It denotes that the upper surface of the airfoil is concave and not convex. ii. An arrangement of the undercarriage in which the wheels are tilted inward of the vertical.… …   Aviation dictionary

  • NACA airfoil — Profile geometry – 1: Zero lift line; 2: Leading edge; 3: Nose circle; 4: Camber; 5: Max. thickness; 6: Upper surface; 7: Trailing edge; 8: Camber mean line; 9: Lower surface …   Wikipedia

  • NACA-Profil — Geometrie eines Profils – 1: Nullauftriebslinie (zero lift line); 2: Flügelnase (leading edge); 3: Krümmungsradius der Flügelnase (nose circle); 4: Skelettlinie (camber); 5: maximale Profildicke (max. thickness); 6: obere Profilseite (upper… …   Deutsch Wikipedia

  • airplane — /air playn /, n. 1. a heavier than air aircraft kept aloft by the upward thrust exerted by the passing air on its fixed wings and driven by propellers, jet propulsion, etc. 2. any similar heavier than air aircraft, as a glider or helicopter. Also …   Universalium

  • Aircraft flight mechanics — In aeronautics, aircraft flight mechanics is the study of the forces that act on an aircraft in flight, and the way the aircraft responds to those forces. [Clancy, L.J. Aerodynamics . Section 14.1] Aircraft flight mechanics are relevant to… …   Wikipedia

  • NACA-Profile — Geometrie eines Profils – 1: Nullauftriebslinie (zero lift line); 2: Flügelnase (leading edge); 3: Krümmungsradius der Flügelnase (nose circle); 4: Wölbung (camber); 5: maximale Profildicke (max. thickness); 6: obere Profilseite (upper surface);… …   Deutsch Wikipedia

  • Angle of attack — In this diagram, the black lines represent the flow of a fluid around a two dimensional airfoil shape. The angle α is the angle of attack. Angle of attack (AOA, α, Greek letter alpha) is a term used in fluid dynamics to describe the angle between …   Wikipedia

  • Gurney flap — The Gurney Flap (or wickerbill) is a small flat tab projecting from the trailing edge of a wing. Typically it is set at a right angle to the pressure side surface of the airfoil,cite journal author = Van Dam, C.P. coauthors = Yen, D.T.; Vijgen, P …   Wikipedia

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