The separated flow method is evaluated. This method was developed for moderately swept wings with multiple, constant strength vortex systems. The flow on the highly swept wing used in this evaluation is characterized by a single vortex system of continuously varying strength.
Aeroelastic loads prediction for an arrow wing. Task 1: Evaluation of R. P. White's method
1983-03-01
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
|