Unsteady supersonic flow calculations for wing-body combinations using harmonic gradient method
- 11 January 1988
- proceedings article
- Published by American Institute of Aeronautics and Astronautics (AIAA)
Abstract
No abstract availableThis publication has 4 references indexed in Scilit:
- Conical, noncircular, second-order, potential theory of supersonic flowAIAA Journal, 1984
- Doublet-Point Method for Supersonic Unsteady Lifting Surfaces.AIAA Journal, 1984
- The Supersonic Triplet-A New Aerodynamic Panel Singularity with Directional PropertiesAIAA Journal, 1980
- Linearized characteristics method for supersonic flow past vibratingshells.AIAA Journal, 1973