Utilization of a free oscillation wind tunnel model in conjunction with an analog computer to determine the dynamic stability derivatives
2nd Aerodynamic Testing Conference ; 1966 ; Los Angeles , CA , U.S.A.
1966-01-01
Aufsatz (Konferenz)
Elektronische Ressource
Englisch
Dynamic Stability Derivatives Evaluation in a Low-Speed Wind Tunnel
Online Contents | 1993
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