Structure of Shock Waves in Cylindrical Ducts
- 1 October 1973
- journal article
- Published by American Institute of Aeronautics and Astronautics (AIAA) in AIAA Journal
- Vol. 11 (10) , 1404-1408
- https://doi.org/10.2514/3.50600
Abstract
No abstract availableThis publication has 4 references indexed in Scilit:
- Precombustion shock structure in scramjet enginesPublished by American Institute of Aeronautics and Astronautics (AIAA) ,1972
- Design of supersonic combustors based on pressure-area fieldsSymposium (International) on Combustion, 1967
- Theoretical Pressure Recovery Through a Normal Shock in a Duct with Initial Boundary LayerJournal of the Aeronautical Sciences, 1953
- Supersonic Diffusers for Wind TunnelsJournal of Applied Mechanics, 1949