Liquid-fueled supersonic combustion ramjets - A research perspective
- 1 November 1987
- journal article
- research article
- Published by American Institute of Aeronautics and Astronautics (AIAA) in Journal of Propulsion and Power
- Vol. 3 (6) , 515-524
- https://doi.org/10.2514/3.23019
Abstract
No abstract availableThis publication has 38 references indexed in Scilit:
- Simultaneous measurements of velocity and pressure fields in subsonic and supersonic flows through image-intensified detection of laser-induced fluorescencePublished by American Institute of Aeronautics and Astronautics (AIAA) ,1986
- A Review of Roughness-Induced Nosetip TransitionAIAA Journal, 1983
- Integral-Rocket Dual-Combustion Ramjets: A New Propulsion ConceptJournal of Spacecraft and Rockets, 1980
- A Procedure for Optimizing the Design of Scrainjet EnginesJournal of Spacecraft and Rockets, 1979
- Pressure Recovery in Rectangular Constant Area Supersonic DiffusersAIAA Journal, 1976
- Wind Tunnel Experiments Relating to Supersonic and Hypersonic Boundary-Layer TransitionAIAA Journal, 1975
- Wall Shear and Boundary-Layer Measurements in Shock Seperated FlowAIAA Journal, 1974
- Structure of Shock Waves in Cylindrical DuctsAIAA Journal, 1973
- Measurements and Correlations of Transition Reynolds Numbers on Sharp Slender Cones at High SpeedsAIAA Journal, 1971
- Supersonic Airfoil Performance with Small Heat AdditionJournal of the Aerospace Sciences, 1959