Recent advances in applying Free Vortex Sheet theory to the estimation of vortex flow aerodynamics
- 11 January 1982
- proceedings article
- Published by American Institute of Aeronautics and Astronautics (AIAA)
Abstract
No abstract availableThis publication has 4 references indexed in Scilit:
- Effect of sweep angles on aerodynamic performance of double arrow wing - An analytical studyJournal of Aircraft, 1981
- Development of a Vortex-Lift Design Procedure and Application to a Slender Maneuver-Wing ConfigurationJournal of Aircraft, 1981
- Nonlinear Prediction of Aerodynamic Loads on Lifting SurfacesJournal of Aircraft, 1976
- Extension of a Vortex-Lattice Method to Include the Effects ofLeading-Edge SeparationJournal of Aircraft, 1974