- thickness/chord ratio of an airfoil section
- відносна товщина профілю крила
Англійсько-український словник авіаційних термінів / Уклад.: Р.О. Гільченко. - К.: НАУ. 2009.
Англійсько-український словник авіаційних термінів / Уклад.: Р.О. Гільченко. - К.: НАУ. 2009.
thickness/chord ratio — The ratio between the maximum thickness or depth of an airfoil section and its chord length, expressed as a percentage of the chord length … Aviation dictionary
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
Aspect ratio (wing) — In aerodynamics, the aspect ratio of a wing is defined as the square of the wing span divided by the wing area.:AR = {b^2 over S}where: b is the wing span, and: S is the wing area.Informally, a high aspect ratio indicates long, narrow wings,… … 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
symmetrical biconvex wing — An airfoil section that is a compromise between the optimum supersonic and subsonic requirements; it has a low thickness/chord ratio for high speed flight and at the same time has curves for low speed work. This type of airfoil has very little… … Aviation dictionary
Supermarine Spitfire — Infobox Aircraft name =Spitfire type =Fighter manufacturer =Supermarine caption =The distinctive silhouette of a typical Spitfire shows elliptical wings. (P7350, a Mk IIa, was first delivered to 266 Squadron on 6 September 1940.) designer =R. J.… … 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
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OMRE OE-01 — OE 1 Role Glider National origin Hungary Manufacturer MRSz Központi Repülögépjavító Üzem, Dunakeszi (Central Aircraft Repair Plant of the MRSz, Dunakeszi) First flight 14 May 1951 Number built 1 The OMRE OE 1 (a.k.a. Rubik R 20) was an ex … 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
Davis wing — The Davis wing is an aircraft wing planform that was used for some time on a variety of World War II aircraft, most notably a number of designs from Consolidated Aircraft, including the Consolidated B 24 Liberator. Use of the Davis wing ended… … Wikipedia