Numerical Study on Abnormal Heat Flux Augmentation in High Enthalpy Shock Tunnel (HIEST)-Reference-Cited by-同舟云学术

Numerical Study on Abnormal Heat Flux Augmentation in High Enthalpy Shock Tunnel (HIEST)

Published:2015 Issue:6 Volume:58 Page:319-326
ISSN:0549-3811
Container-title:TRANSACTIONS OF THE JAPAN SOCIETY FOR AERONAUTICAL AND SPACE SCIENCES
language:en
Short-container-title:Trans. Japan Soc. Aero. S Sci.

Author:

ISHIHARA Tomoaki¹,OGINO Yousuke¹,OHNISHI Naofumi¹,TANNO Hideyuki²

Affiliation:

1. Department of Aerospace Engineering, Tohoku University

2. Kakuda Space Center, Japan Aerospace Exploration Agency

Publisher

Japan Society for Aeronautical and Space Sciences

Subject

Space and Planetary Science,Aerospace Engineering

Link

https://www.jstage.jst.go.jp/article/tjsass/58/6/58_T-14-85/_pdf

Reference23 articles.

1. 1) Tanno, H., Kodera, M., Komura, T., Sato, K., Takahashi, M., and Itoh, K.: Aeroheating Measurements on a Reentry Capsule Model in Free-Piston Shock Tunnel HIEST, AIAA Paper 2010-1181, 2010.

2. 2) Ishihara, T., Ogino, Y., Sawada, K., and Tanno, H.: Computation of Surface Heat Transfer Rate on Apollo CM Test Model in Free-Piston Shock Tunnel HIEST, AIAA Paper 2012-0285, 2012.

3. 3) Hollis, B. R. and Praha, D. K.: Assessment of Laminar, Convective Aeroheating Prediction Uncertainties for Mars Entry Vehicles, AIAA Paper 2011-3144, 2011.

4. 4) Stewart, D. A. and Chen, Y. K.: Hypersonic Convective Heat Transfer over 140-deg Blunt Cones in Different Gases, J. Spacecraft Rockets, 31, 5 (1994), pp. 735–743.

5. 5) Marineau, C. E., Laurence, S. J., and Hornung, H. G.: Apollo-Shaped Capsule Boundary Layer Transition at High Enthalpy in T5, AIAA Paper 2010-446, 2010.

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