Characteristics procedure for supersonic flows including consideration of viscous contributions to flow rotationality
- 14 July 1976
- proceedings article
- Published by American Institute of Aeronautics and Astronautics (AIAA)
Abstract
No abstract availableThis publication has 1 reference indexed in Scilit:
- Finite difference procedure for boundary layers including effects oflongitudinal and transverse curvaturesPublished by American Institute of Aeronautics and Astronautics (AIAA) ,1976