Effects of Mach number and afterbody length on aerodynamic side forces at zero sideslip on symmetric bodies at high angles of attack
14th Aerospace Sciences Meeting ; 1976 ; Washington , DC , U.S.A.
01.01.1976
Aufsatz (Konferenz)
Elektronische Ressource
Englisch
Wind Tunnel Aerodynamic Study of a VTOL-UAV for Wide Range of Angles of Attack and Sideslip Angles
Springer Verlag | 2021
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