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