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
148 pages
Report
Keine Angabe
Englisch
Prediction analysis techniques , Mathematical models , Aerodynamic characteristics , Boundary layer flow , Computerized simulation , Aerodynamics , Aircraft , V/stol aircraft , Viscous flow , Computer Aided Design, CAD , Jet propulsion , Nacelles , Computer aided design , Computer programs , Aerodynamic configurations