- chord/thickness ratio
- Авиация: относительная толщина профиля
Универсальный англо-русский словарь. Академик.ру. 2011.
chord/thickness ratio
Смотреть что такое "chord/thickness ratio" в других словарях:
thickness ratio — noun : the ratio of the maximum thickness of an airfoil to the chord at that station … Useful english dictionary
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
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
fineness ratio — The ratio of the chord to the maximum thickness of an airfoil expressed as a percentage. In the case of other streamlined bodies, it is the ratio of their length to their maximum diameter, or, sometimes, to some equivalent dimension. This is said … Aviation dictionary
propeller camber ratio — The ratio of the maximum thickness of a blade to its chord at any station … Aviation dictionary
Vickers Valiant — For other uses see: Valiant infobox Aircraft name = Vickers Valiant type = Strategic bomber manufacturer =Vickers Armstrongs caption =RAF Valiant in anti flash white designer = first flight =18 May avyear|1951 introduced =1955 retired =January… … Wikipedia
Dyle et Bacalan DB-70 — DB 70 Role Airliner National origin France Manufacturer Dyle et Bacalan (Société Anonyme de Travaux Dyle et Bacalan), Bordeaux Designer M.L. de Monge[1] First flight … Wikipedia
Lockheed P-38 Lightning — P 38 redirects here. For other uses, see P 38 (disambiguation). P 38 Lightning P 38H 5 LO, AAF Ser. No. 4 … Wikipedia
P-38 Lightning — infobox Aircraft name =P 38 Lightning type =Heavy fighter manufacturer =Lockheed caption = designer =Kelly Johnson first flight =27 January 1939 introduction = 1941 retired = 1949 primary user = United States Army Air Force more users = produced … 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
Camber (aerodynamics) — Camber, in aerospace engineering, is the asymmetry between the top and the bottom curves of an airfoil in cross section.OverviewCamber is often added to an airfoil to increase lift and/or reduce the critical angle of attack (the angle at which… … Wikipedia
