Internal flow calculations for axisymmetric supersonic inlets at angle of attack
- 16 August 1975
- conference paper
- Published by American Institute of Aeronautics and Astronautics (AIAA)
Abstract
No abstract availableThis publication has 3 references indexed in Scilit:
- On the shock-on-shock interaction problemPublished by American Institute of Aeronautics and Astronautics (AIAA) ,1974
- A comparison of numerical solutions to the inviscid equations of fluid motionJournal of Computational Physics, 1974
- COMPARISON OF A DISCRETE-SHOCK, FINITE-DfFFEf^tNCi^ 1ECHNIQUE AND THE METHOD OF CHARACTERISTICS FOR CALCULATING INTERNAL SUPERSONIC FLOWSPublished by American Institute of Aeronautics and Astronautics (AIAA) ,1973