Calculation of unsteady transonic flows with shocks by field panel methods
- 1 June 1982
- journal article
- Published by American Institute of Aeronautics and Astronautics (AIAA) in AIAA Journal
- Vol. 20 (6) , 857-859
- https://doi.org/10.2514/3.7949
Abstract
No abstract availableKeywords
This publication has 4 references indexed in Scilit:
- Wing-body carryover at supersonic speeds with finite afterbodiesAIAA Journal, 1981
- Calculation of transonic flow by means of a shock-capturing field panel methodPublished by American Institute of Aeronautics and Astronautics (AIAA) ,1979
- Calculation of unsteady transonic flows using the integral equation methodPublished by American Institute of Aeronautics and Astronautics (AIAA) ,1978
- ANALYSIS OF EMBEDDED SHOCK WAVES CALCULATED BY RELAXATION METHODSPublished by American Institute of Aeronautics and Astronautics (AIAA) ,1973