Experimental and numerical study of swept ramp injection into a supersonic flowfield
Author:
Affiliation:
1. University of Virginia, Charlottesville, Virginia 22903
Publisher
American Institute of Aeronautics and Astronautics (AIAA)
Subject
Aerospace Engineering
Link
http://arc.aiaa.org/doi/pdf/10.2514/3.12184
Reference16 articles.
1. Experimental investigation of a supersonic swept ramp injector using laser-induced iodine fluorescence
2. A numerical study of mixing enhancement in a supersonic combustor
3. Investigation of a contoured wall injector for hypervelocity mixing augmentation
4. Analysis of losses in supersonic mixing and reacting flows
5. Computational/experimental investigation of staged injection into a Mach 2 flow
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