Measurement of shock stand-off distance for sphere in ballistic range-Reference-Cited by-同舟云学术

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Measurement of shock stand-off distance for sphere in ballistic range

Published:1997-01-06 Issue: Volume: Page:
ISSN:
Container-title:35th Aerospace Sciences Meeting and Exhibit
language:
Short-container-title:

Author:

Nonaka Satoshi¹,Takayama Kazuyoshi¹,Park Chul¹,Nonaka Satoshi¹,Takayama Kazuyoshi¹,Park Chul¹

Affiliation:

1. Tohoku Univ., Sendai, Japan

Publisher

American Institute of Aeronautics and Astronautics

Link

http://arc.aiaa.org/doi/pdf/10.2514/6.1997-563

Reference12 articles.

1. Assessment of two-temperature kinetic model for ionizing air

2. Hornung, H. G., and Wen, C. Y. "Nonequilibrium Dissociating Flow Over Spheres," AIAAPaper 95-0091,1995.

3. Skinner, K. A. "Mass Spectrometry in Shock Tunnel Experiments of Hypersonic Combustion," Ph.D. Thesis,University of Queensland, Australia, 1994.

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. Wave dynamic processes induced by a supersonic projectile discharging from a shock tube;Physics of Fluids;2003

2. Validation of hypersonic equilibrium flow calculations using ballistic-range data;35th Aerospace Sciences Meeting and Exhibit;1997-01-06

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