Effects of thermal compression on the performance estimates of hypersonic ramjets.
- 1 September 1968
- journal article
- Published by American Institute of Aeronautics and Astronautics (AIAA) in Journal of Spacecraft and Rockets
- Vol. 5 (9), 1076-1081
- https://doi.org/10.2514/3.29424
Abstract
No abstract availableKeywords
This publication has 2 references indexed in Scilit:
- Design of supersonic combustors based on pressure-area fieldsSymposium (International) on Combustion, 1967
- Notes on the Rapid Computation of Chemical EquilibriaThe Journal of Physical Chemistry, 1964