- canard-tail configuration
- схема "утка" <ракеты>
Авиасловарь. М.А.Левин. 2004.
Авиасловарь. М.А.Левин. 2004.
Configuration d'aile — Réplique du Fokker Dr.I, triplan piloté par le Baron rouge lors de la Première Guerre mondiale. Depuis les débuts de l aviation, de nombreuses configurations d aile ont été imaginées pour permettre aux « plus lourds que l air » – d… … Wikipédia en Français
Canard (aeronautics) — In aeronautics, canard (French for duck) is an airframe configuration of fixed wing aircraft in which the tailplane is ahead of the main wing, rather than behind them as in conventional aircraft.Crane, Dale: Dictionary of Aeronautical Terms,… … Wikipedia
Canard Rotor/Wing — The Canard Rotor Wing (CRW) is a class of VTOL aircraft capable of both fixed wing and rotary wing flight. For vertical take off, hovering, low speed flight, and vertical landing, the main airfoil is spun like a helicopter s rotor by directing… … Wikipedia
Wing configuration — For aircraft configurations in general, including fuselage, tail and powerplant configuration, see Aircraft. For rotary winged aircraft types, see Rotorcraft. For direct lift and compound or hybrid types, see Powered lift. Fixed wing aircraft,… … Wikipedia
Pusher configuration — An aircraft constructed with a pusher configuration has the engine mounted forward of the propeller which faces in a rearwards direction giving an appearance that the aircraft is pushed through the air. Sometimes the propeller is situated at the… … Wikipedia
dart configuration — A configuration of an aerodynamic vehicle in which the control surfaces are at the tail of the vehicle. This is the reverse of the canard configuration. Laser guided weapons are of a dart configuration. See also canard configuration. See laser… … Aviation dictionary
Cruciform tail — BAe Jetstream 31 with cruciform tail The cruciform tail is an aircraft empennage configuration which, when viewed from the aircraft s front or rear, looks much like a cross. The usual arrangement is to have the horizontal stabilizer intersect the … 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
Ambrosini SS.4 — infobox Aircraft name = Ambrosini SS.4 type =Fighter manufacturer = SAI Ambrosini caption = Three views of the SS.4 designer = Sergio Stefanutti first flight = 1935 number built = 3(?) status =prototype primary user =Regia Aeronautica The SAI… … Wikipedia
Supermaneuverability — is quality of aircraft defined as a threshold of attitude control exceeding that which is possible by pure aerodynamic maneuverability. It is a trait of some advanced fourth generation and 4.5 generation fighter aircraft and is generally a… … Wikipedia
USAF Digital DATCOM — The United States Air Force Stability and Control Digital DATCOM is a computer program that implements the methods contained in the USAF Stability and Control DATCOM to calculate the static stability, control and dynamic derivative… … Wikipedia