The integral-rocket, dual-combustion ramjet - A new propulsion concept
- 1 April 1979
- proceedings article
- Published by American Institute of Aeronautics and Astronautics (AIAA)
Abstract
No abstract availableThis publication has 6 references indexed in Scilit:
- Structure of Shock Waves in Cylindrical DuctsAIAA Journal, 1973
- Prediction of Precombustion Wall Pressure Distributions in Scramjet EnginesJournal of Spacecraft and Rockets, 1973
- 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