Design, Fabrication, Testing, and Data Analysis of Adam II Concept (Propulsive Wing). Part III, Testing in 17 Ft Test Section of 7 Ft X 10 Ft Wind Tunnel, NASA Langley Research Center
1968
105 pages
Report
Keine Angabe
Englisch
Aircraft , Fluid Mechanics , Vertical takeoff aircraft , Aerodynamic characteristics , Aerodynamic control surfaces , Ground effect , Interference , Wind tunnel models , Models(Simulations) , Model tests , Scale , Aerodynamic configurations , Gas generating systems , Hovering , Stability , Thrust , Design , Subsonic characteristics , Transonic characteristics , Level flight , Test facilities , Test equipment , Air deflection and modulation , Adam(Air deflection and modulation) , Adam 2 aircraft , Transition flight
Applications of Modern Experiment Design to Wind Tunnel Testing at NASA Langley Research Center
British Library Conference Proceedings | 1998
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