An Investigation at Mach Numbers from 0.40 to 1.00 of a Model with a Wing Having Inboard Sections Cambered for Mach 1.2
1966
41 pages
Report
Keine Angabe
Englisch
Aerodynamics , Aerodynamic characteristics , Aircraft model , Longitudinal stability , Subsonic speed , Wing body , Aerodynamic , Aircraft , Body , Chamber , Characteristics , Longitudinal , Model , Speed , Stability , Subsonic , Tail , Test , Transport , Tunnel , Wind , Wing
Engineering Index Backfile | 1948
|Engineering Index Backfile | 1949
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