The development and evaluation of a semi empirical method to predict pressure distributions on a deformed wing by using an experimental data base in addition to a linear potential flow solution is described. The experimental data accounts for the effects of aeroelasticity by relating the pressures to a parameter which is influenced by the deflected shape. Several parameters were examined before the net leading edge suction coefficient was selected as the best.
Aeroelastic Loads Prediction for an Arrow Wing. Task 2: Evaluation of Semi-Empirical Methods
1983
123 pages
Report
No indication
English
Static Aeroelastic Effects Upon Wing Span Loads
British Library Conference Proceedings | 1991
|Static aeroelastic effects upon wing span loads
AIAA | 1991
|