Characterization of Shock Train Structures inside Constant-Area Isolators of Model Scramjet Combustors
Author:
Affiliation:
1. Taitech, Inc.
2. U.S. Air Force Research Laboratory
Publisher
American Institute of Aeronautics and Astronautics
Link
http://arc.aiaa.org/doi/pdf/10.2514/6.2006-816
Reference7 articles.
1. Structure of Shock Waves in Cylindrical Ducts
2. Prediction of Precombustion Wall Pressure Distributions in Scramjet Engines
3. Sullins, G., and McLafferty, G. "Experimental Results of Shock Trains in Rectangular Ducts," AIAA Paper92-5103, December1992.
4. White, J. A. and Morrison, J. H. "A Pseudo-Temporal Multi-Grid Relaxation Scheme for Solving the ParabolizedNavier-Stokes Equations,"AIAA Paper99-3360, June1999.
5. A low-diffusion flux-splitting scheme for Navier-Stokes calculations
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