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 prediction methods are suitable for use by design personnel during the preliminary design and evaluation of V/STOL aircraft of the type previously mentioned. The results of a literature survey are presented in this volume. (Author)
V/STOL Aircraft Aerodynamic Prediction Methods Investigation. Volume IV. Literature Survey
1972
78 pages
Report
Keine Angabe
Englisch
Aircraft , Aerodynamics , Aerodynamic characteristics , Short take-off planes , Mathematical prediction , Vertical take-off planes , Flow fields , Lift , Flow separation , Vortices , Wake , Stalling , Interactions , Abstracts , Bibliographies , Computer aided analysis , Computer aided design , Design criteria