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.
1980-01-01
Conference paper
Electronic Resource
English
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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