A Study to Determine Effects of Applying Thrust on Recovery from Incipient and Developed Spins for Four Airplane Configurations
1966
49 pages
Report
No indication
English
Aerodynamics , Aerodynamic stability , Aircraft configuration , Control surface , Thrust effect , Aerodynamic , Aircraft , Configuration , Control , Deflection , Delta , Effect , Incipient , Optimal , Oscillation , Recovery , Spin , Surface , Sweep , Thrust , Wing
Engineering Index Backfile | 1930
|Engineering Index Backfile | 1930
|