Determination of an angle of attack sensor correction for a general aviation airplane at large angles of attack as determined from wind tunnel and flight tests
Aircraft Systems Meeting ; 1980 ; Anaheim , CA , U.S.A.
01.01.1980
Aufsatz (Konferenz)
Elektronische Ressource
Englisch
Wind tunnel force tests in wing systems through large angles of attack
Engineering Index Backfile | 1928
|Wind-Tunnel Investigation of a General-Aviation Differential Pressure Angle-of-Attack Probe
Online Contents | 2013
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