thrust deflection
31Vought F-8 Crusader — F 8 redirects here. For other uses, see F8 (disambiguation). F 8 (F8U) Crusader An F 8E from VMF(AW) 212 in …
32Spring (device) — Helical or coil springs designed for tension Compression sp …
33A-10 Thunderbolt II — Infobox Aircraft name = A 10 Thunderbolt II type = Close air support attack aircraft manufacturer = Fairchild Republic caption = designer = first flight =10 May 1972 introduction =March 1977 retired = number built =715 [… …
34North American A-5 Vigilante — A 5 (A3J) Vigilante Role Nuclear strike bomber, reconnaissance aircraft Manufacturer North American Aviation …
35Wing loading — In aerodynamics, wing loading is the loaded weight of the aircraft divided by the area of the wing. [Thom, 1988. p. 6.] It is broadly reflective of the aircraft s lift to mass ratio, which affects its rate of climb, load carrying ability, and… …
36Radio-controlled aircraft — A radio controlled aircraft (often called RC aircraft or RC plane) is a model aircraft that is controlled remotely, typically with a hand held transmitter and a receiver within the craft. The receiver controls the corresponding servos that move… …
37Autoland — In aviation, autoland describes a system that fully automates the landing phase of an aircraft s flight, with the human crew merely supervising the process.DescriptionAutoland systems were designed to make landing possible in visibility too poor… …
38Deflected slipstream — is an approach to creating an aircraft that can take off and land vertically (VTOL), or at least with a very short runway (STOL). The basic principle is to deflect the slipstream from one or more propellers approximately 90 degrees, to create an… …
39Cornering force — Tire tread element displacement and the resulting cornering force Cornering force or side force is the lateral (i.e. parallel to the road surface) force produced by a vehicle tire during cornering.[1] Cornering force is generated by tire slip and …
40Stability derivatives — are a means of linearising the equations of motion of an atmospheric flight vehicle so that conventional control engineering methods may be applied to assess their stability.The dynamics of atmospheric flight vehicles is potentially very… …
