A Prismatic Grid Generation Method Suitable for Predicting Aerodynamic Characteristics of Winged Re-entry Vehicles-Reference-Cited by-同舟云学术

A Prismatic Grid Generation Method Suitable for Predicting Aerodynamic Characteristics of Winged Re-entry Vehicles

Published:2022 Issue:5 Volume:70 Page:152-161
ISSN:1344-6460
Container-title:JOURNAL OF THE JAPAN SOCIETY FOR AERONAUTICAL AND SPACE SCIENCES
language:en
Short-container-title:JOURNAL OF THE JAPAN SOCIETY FOR AERONAUTICAL AND SPACE SCIENCES

Author:

Okano Yasuhito¹,Kuya Yuichi²,Sawada Keisuke³,Tanno Hideyuki⁴

Affiliation:

1. 連絡先著者(Corresponding author)：yasuhito.okano.p4@dc. tohoku.ac.jp

2. 東北大学大学院工学研究科航空宇宙工学専攻

3. 国立高等専門学校機構仙台高等専門学校

4. 宇宙航空研究開発機構角田宇宙センター

Publisher

Japan Society for Aeronautical and Space Sciences

Subject

General Medicine

Link

https://www.jstage.jst.go.jp/article/jjsass/70/5/70_70_152/_pdf

Reference32 articles.

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2. 2) Candler, G. V.: Rate Effects in Hypersonic Flows, Annu. Rev. Fluid Mech., 51 (2019), pp. 379-402.

3. 3) Maus, J. R., Griffith, B. J. and Szema, K. Y.: Hypersonic Mach Number and Real Gas Effects on Space Shuttle Orbiter Aerodynamic, J. Spacecr. Rockets, 21 (1984), pp. 136-141.

4. 4) Griffith, B. J., Maus, J. R. and Majors, B. M.: Addressing the Hypersonic Simulation Problem, J. Spacecr. Rockets, 24 (1987), pp. 334-341.

5. 5) Kristen, W. P., Richardson, D. F. and Wilson, C. M.: Predicted and Flight Test Results of the Performance, Stability and Control of the Space Shuttle from Reentry to Landing, NASA Langley Research Center Suttle Performance: Lessons Learned, Part 1, 1983, pp. 509-524.