Hypersonic Type-IV Shock/Shock Interactions on a Blunt Body with Forward-Facing Cavity-Reference-Cited by-同舟云学术

Hypersonic Type-IV Shock/Shock Interactions on a Blunt Body with Forward-Facing Cavity

Published:2017-03 Issue:2 Volume:54 Page:506-512
ISSN:0022-4650
Container-title:Journal of Spacecraft and Rockets
language:en
Short-container-title:Journal of Spacecraft and Rockets

Author:

Xiao Fengshou¹,Li Zhufei¹,Zhu Yujian¹,Yang Jiming¹

Affiliation:

1. University of Science and Technology of China, 230026 Hefei, People’s Republic of China

Funder

National Natural Science Foundation of China

Publisher

American Institute of Aeronautics and Astronautics (AIAA)

Subject

Space and Planetary Science,Aerospace Engineering

Link

https://arc.aiaa.org/doi/pdf/10.2514/1.A33556

Reference22 articles.

1. WattsJ. D. “Flight Experience with Shock Impingement and Interference Heating on the X-15-2 Research Airplane,” NASA TM X-1669, 1968.

2. 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, Stockholm, Sweden, Feb. 1968.

3. Experimental shock-wave interference heating on a cylinder at Mach 6and 8

4. Studies of aerothermal loads generated in regions of shock/shock interaction in hypersonic flow

5. KollyJ. M. “An Investigation of Aerothermal Loads Generated in Regions of Hypersonic Shock Interference Flows,” Ph.D. Dissertation, State Univ. of New York at Buffalo, Buffalo, NY, 1996.

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