Ballistic range measurement of shock shapes in intermediate hypersonic regime-Reference-Cited by-同舟云学术

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Ballistic range measurement of shock shapes in intermediate hypersonic regime

Published:1999-01-11 Issue: Volume: Page:
ISSN:
Container-title:37th Aerospace Sciences Meeting and Exhibit
language:
Short-container-title:

Author:

Nonaka Satoshi¹,Mizuno Hiroyasu¹,Takayama Kazuyoshi¹

Affiliation:

1. Tohoku Univ., Sendai, Japan

Publisher

American Institute of Aeronautics and Astronautics

Link

http://arc.aiaa.org/doi/pdf/10.2514/6.1999-1025

Reference23 articles.

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

2. Validation of CFD codes for real-gas regime

Cited by 9 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. Theoretical investigation of shock stand-off distance for non-equilibrium flows over spheres;Chinese Journal of Aeronautics;2018-05

2. Calculation of Shock Shapes over Sharp Cone in Intermediate Hypersonic Airflow;Journal of Thermophysics and Heat Transfer;2003-04

3. Three-dimensional calculations of hypersonic flowfield over double-cone geometries;40th AIAA Aerospace Sciences Meeting & Exhibit;2002-01-14

4. Effect of rotational nonequilibrium on shock standoff distances;39th Aerospace Sciences Meeting and Exhibit;2001-01-08

5. Effects of Vibrational Relaxation on Bow Shock Standoff Distance for Nonequilibrium Flows;AIAA Journal;2000-09

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