A Procedure for Optimizing the Design of Scrainjet Engines
- 1 May 1979
- journal article
- Published by American Institute of Aeronautics and Astronautics (AIAA) in Journal of Spacecraft and Rockets
- Vol. 16 (3) , 163-171
- https://doi.org/10.2514/3.57637
Abstract
No abstract availableKeywords
This publication has 7 references indexed in Scilit:
- Direct-connect tests of hydrogen-fueled supersonic combustorsSymposium (International) on Combustion, 1977
- Prediction of Precombustion Wall Pressure Distributions in Scramjet EnginesJournal of Spacecraft and Rockets, 1973
- Curve fits of JANAF thermochemical dataPublished by Office of Scientific and Technical Information (OSTI) ,1972
- HEAT TRANSFER IN SUPERSONIC COMBUSTION PROCESSESPublished by Begell House ,1970
- The interaction of shock waves and heat addition in the design of supersonic combustorsSymposium (International) on Combustion, 1969
- 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