Analytical engineering methods are developed for use in predicting the static and dynamic stability and control derivatives and force and moment coefficients of lift-jet, lift-fan, and vectored thrust V/STOL aircraft in the hover and transition flight regimes. The aircraft configurations studied have a conventional wing, fuselage and empennage. The prediction methods are applied to a number of V/STOL configurations in this volume. (Author)
V/STOL Aircraft Aerodynamic Prediction Methods Investigation. Volume II. Application of Prediction Methods
1972
248 pages
Report
Keine Angabe
Englisch
Aircraft , Aerodynamics , Aerodynamic characteristics , Short take-off planes , Mathematical prediction , Vertical take-off planes , Flow fields , Lift , Predictions , Flow separation , Vortices , Wake , Stalling , Interactions , Mathematical models , Mapping(Transformations) , Computer aided analysis , Computer aided design , Design criteria