Numerical investigation of the effects of blowing on high angle of attack flow over delta wings
- 24 June 1991
- conference paper
- Published by American Institute of Aeronautics and Astronautics (AIAA)
Abstract
No abstract availableThis publication has 1 reference indexed in Scilit:
- Analysis of Viscous Flowfield Over Tactical Aircraft Forebody and InletsPublished by ASME International ,1990