airfoil leading edge thickness

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• Airfoil — An airfoil (in American English) or aerofoil (in British English) is the shape of a wing or blade (of a propeller, rotor or turbine) or sail as seen in cross section. An airfoil shaped body moved through a fluid produces a force perpendicular to… …   Wikipedia

• 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 (National Advisory Committee for Aeronautics) airfoil — A method of indicating characteristics of an airfoil. This can be done by describing the airfoil using 4, 5, 6, 7, or 8 digits. In a NACA 4 digit airfoil, the first digit expresses the camber in the percentage of chord, the second digit gives the …   Aviation dictionary

• толщина входной кромки пера — толщина входной кромки C1 Толщина профиля пера на длине входной кромки пера. [ГОСТ 23537 79] Тематики авиационные компрессоры и трубины Обобщающие термины параметры лопатки и ее элементов Синонимы толщина входной кромки EN airfoil leading edge… …   Справочник технического переводчика

• fluid mechanics — an applied science dealing with the basic principles of gaseous and liquid matter. Cf. fluid dynamics. [1940 45] * * * Study of the effects of forces and energy on liquids and gases. One branch of the field, hydrostatics, deals with fluids at… …   Universalium

• Lift (force) — For other uses, see Lift. Boeing 747 8F landing A fluid flowing past the surface of a body exerts a surface force on it. Lift is the component of this force that is perpendicular to the …   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

• 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

• Stall (flight) — For other uses, see stall. In fluid dynamics, a stall is a reduction in the lift coefficient generated by a foil as angle of attack increases. This occurs when the critical angle of attack of the foil is exceeded. The critical angle of attack is… …   Wikipedia

• Hawker Tempest — infobox Aircraft name = Hawker Tempest type = Fighter/Bomber manufacturer = Hawker Aircraft Limited caption = A late production Hawker Tempest V. designer =Sydney Camm first flight = 2 September 1942 introduced = January 1944 retired = status =… …   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