Influence of nonconservative differencing on transonic streamline shapes
- 1 August 1976
- journal article
- Published by American Institute of Aeronautics and Astronautics (AIAA) in AIAA Journal
- Vol. 14 (8) , 1148-1149
- https://doi.org/10.2514/3.7208
Abstract
No abstract availableKeywords
This publication has 3 references indexed in Scilit:
- ANALYSIS OF EMBEDDED SHOCK WAVES CALCULATED BY RELAXATION METHODSPublished by American Institute of Aeronautics and Astronautics (AIAA) ,1973
- Analysis of transonic airfoilsCommunications on Pure and Applied Mathematics, 1971
- Calculation of plane steady transonic flowsAIAA Journal, 1971