The parametric analysis and experimental investigation of sidewall compression inlet at Mach 5.3 in non-uniform incoming flow condition-Reference-Cited by-同舟云学术

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The parametric analysis and experimental investigation of sidewall compression inlet at Mach 5.3 in non-uniform incoming flow condition

Published:1995-07-10 Issue: Volume: Page:
ISSN:
Container-title:31st Joint Propulsion Conference and Exhibit
language:
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Author:

Zhang Kun,Xiao Xu,Xu Hui

Publisher

American Institute of Aeronautics and Astronautics

Link

http://arc.aiaa.org/doi/pdf/10.2514/6.1995-2889

Reference16 articles.

1. Trexler Car A. :Performance of an Inlet for an Integrated ScramjetConcept. J. AircraftVol 11, No. 9 1974.

2. Lawing. P. L. :Inlet Boundary Layer Shapes on Four Aircraft Forebodies at Mach 6. J. Aircraft. Vol. 15. No. 1. 1978.

Cited by 2 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. Analysis of Flows in Scramjet Isolator Combined with Hypersonic Inlet;43rd AIAA Aerospace Sciences Meeting and Exhibit;2005-01-10

2. Three-Dimensional Sidewall-Compression Scramjet Inlet CFD Simulation and Experimental Comparison;39th AIAA/ASME/SAE/ASEE Joint Propulsion Conference and Exhibit;2003-06-26

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