Navier-Stokes analysis of supersonic flow over a rearward facing step followed by two jets-Reference-Cited by-同舟云学术

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Navier-Stokes analysis of supersonic flow over a rearward facing step followed by two jets

Published:1995-01-09 Issue: Volume: Page:
ISSN:
Container-title:33rd Aerospace Sciences Meeting and Exhibit
language:
Short-container-title:

Author:

Warfield Matthew

Publisher

American Institute of Aeronautics and Astronautics

Link

http://arc.aiaa.org/doi/pdf/10.2514/6.1995-520

Reference13 articles.

1. Fo 4611-86-C-0087with OL-ACPhillips Laboratory,

2. Warfield, Matthew J. and Henke, Robert K. "Navier-StokesAnalysisofIntegratedRocketBody andPlumeFlowfieldswith Chemisuy",AIAA-89-2896, 1989

3. Holcomb,J. E. "Three-DimensionalNavier-Stokes RocketPlumeCalculations",AIAA-89-1986,1989

4. Holden, Michael S., Nowak, Robert J., Olsen, George C., and Rodriguez, Kathleen M., 12. Holcomb,J. E. "3-DAdaptiveGridNavier-Stokes "Experimental Studies of Shock Wave/Wall Jet Interaction in HypersonicFlow", AIAA 90-0607, January,1990 RocketPlumeCalculations",AIAA-91,0146,1991

5. Warfield, M. J. "Calculation of Supersonic InteractingJet Flows,'' AIAA-89-0666,January,

Cited by 1 articles. 订阅此论文施引文献订阅此论文施引文献，注册后可以免费订阅5篇论文的施引文献，订阅后可以查看论文全部施引文献

1. Experimental and analytical investigation of injection behind a pylon in a compressible flow;34th Aerospace Sciences Meeting and Exhibit;1996-01-15

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