Effects of nozzle geometry on parallel injection from the base of an extended strut into a supersonic flow
Author:
Publisher
American Institute of Aeronautics and Astronautics
Link
http://arc.aiaa.org/doi/pdf/10.2514/6.1995-522
Reference18 articles.
1. Advanced injection and mixing techniques for scramjet combustors
2. Study of compressible mixing layers using filtered Rayleigh scattering based visualizations
3. Mixing studies of helium in air at high supersonic speeds
4. Glawe, D.G. (to be completed Summer 1995) The Effects of Nozzle Geometry on Parallel Injection from the Base of an Extended Strut into a Supersonic Freestream. Ph.D Dissertation, OSU DepartmentofMechanicalEngineering.
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