The V/STOL Aircraft Propulsive Effects (VAPE) computerized prediction method is evaluated. The program analyzes viscous effects, various jet, inlet, and Short TakeOff and Landing (STOL) models, and examines the aerodynamic configurations of V/STOL aircraft.
Advanced prediction technique for the low speed aerodynamics of V/STOL aircraft. Volume 1: Technical discussion
1984-03-15
Report
No indication
English