Influence of Hypersonic Inlet Cowl Lip on Flowfield Structure and Thermal Load-Reference-Cited by-同舟云学术

Influence of Hypersonic Inlet Cowl Lip on Flowfield Structure and Thermal Load

Published:2014-09 Issue:5 Volume:30 Page:1175-1182
ISSN:0748-4658
Container-title:Journal of Propulsion and Power
language:en
Short-container-title:Journal of Propulsion and Power

Author:

Weixing Wang¹,Rongwei Guo¹

Affiliation:

1. College of Energy and Power Engineering, JiangSu Province Key Laboratory of Aerospace Power System, Nanjing University of Aeronautics and Astronautics, 210016 Nanjing, JiangSu, People’s Republic of China

Publisher

American Institute of Aeronautics and Astronautics (AIAA)

Subject

Space and Planetary Science,Mechanical Engineering,Fuel Technology,Aerospace Engineering

Link

http://arc.aiaa.org/doi/pdf/10.2514/1.B35138

Reference14 articles.

1. AIAA Education Series;Bertin J. J.,1994

2. RyanB. M. “Summary of the Aerothermodynamic Interference Literature,” U.S. Naval Weapons Center TN 4061-160, China Lake, CA, April 1969.

3. Survey of viscous interactions associated with high Mach number flight

4. KeyesJ. W.HainsF. D. “Analytical and Experimental Studies of Shock Interference Heating in Hypersonic Flow,” NASA TN D-7139, May 1973.

5. EdneyB. “Anomalous Heat Transfer and Pressure Distributions on Blunt Bodies at Hypersonic speeds in the Presence of an Impinging Shock,” Aeronautical Research Inst. of Sweden, FFA Rept. 115, Bromma, Sweden, 1968.

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