stalling characteristics
1Stall (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… …
2British European Airways Flight 548 — Infobox Aircraft accident|name=British European Airways Flight 548 Crash Date=18 June 1972 Type=Deep stall aircraft misconfiguration caused by pilot error Site=Staines, England Fatalities=118 Injuries=0 Aircraft Type=Hawker Siddeley Trident 1C… …
3de Havilland DH.34 — DH.34 Role Airliner Manufacturer de Havilland Designer Geoffrey de Havi …
4North American P-51 Mustang — P 51 redirects here. For other uses, see P51 (disambiguation). P 51 Mustang P 51 Mustangs of the 375th Fighter Squadron, 361st Fighter Group …
5Dan-Air — For the Danish airline, see Danair. Dan Air Services IATA DA ICAO DAN Callsign …
6Short Sherpa — This article is about the SB.4 Sherpa, for the C 23 Sherpa transport, see C 23 Sherpa infobox Aircraft name=SB.4 Sherpa type=Experimental aircraft manufacturer=Short Brothers caption=Short Sherpa flown by the College of Aeronautics at Cranfield c …
7De Havilland DH.34 — infobox Aircraft name = D.H.34 type = Airliner manufacturer = de Havilland caption = designer = Geoffrey de Havilland first flight = 1922 introduced = 1922 retired = 1926 primary user = Imperial Airways more users = Daimler Hire Ltd Instone Air… …
8de Havilland Hornet — For the 1930s single engine cabin biplane see: de Havilland Hornet Moth D.H.103 Hornet Sea Hornet A de Havilland Ho …
9De Havilland Hornet — For the 1930 s single engine cabin biplane see: de Havilland Hornet Moth infobox Aircraft name = D.H.103 Hornet Sea Hornet type = Land and naval based fighter aircraft manufacturer = de Havilland caption = The de Havilland Hornet Mk 1 (F.1)(note… …
10Clark Y — is the name of a particular aerofoil profile, widely used in general purpose aircraft designs, and much studied in aerodynamics over the years. The profile was designed in 1922 by Virginius E. Clark. The airfoil has a thickness of 11.7 percent… …
