Wind tunnel tests of stability and control characteristics of large scale model representative of propeller-driven STOL transport aircraft
Stability and control characteristics of a large scale deflected slipsteam STOL model with a wing of 5.7 aspect ratio
1971-10-01
Sonstige
Keine Angabe
Englisch
Canadair tilt-wing/deflected slipstream V/STOL prototype program
Engineering Index Backfile | 1964
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