3-Dimensional Numerical Simulation of Hypersonic Intake for Pre-Cooled Turbo Jet Engine
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Published:2021
Issue:5
Volume:19
Page:676-681
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ISSN:1884-0485
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Container-title:TRANSACTIONS OF THE JAPAN SOCIETY FOR AERONAUTICAL AND SPACE SCIENCES, AEROSPACE TECHNOLOGY JAPAN
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language:en
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Short-container-title:AEROSPACE TECHNOLOGY JAPAN
Author:
SANO Masakazu1, YOKOI Toshiya1, YOSHIDA Hidekazu1, SATO Tetsuya1, TAGUCHI Hideyuki2
Affiliation:
1. Department of Applied Mechanics, Waseda University 2. Aeronautical Technology Directorate, JAXA
Publisher
Japan Society for Aeronautical and Space Sciences
Reference22 articles.
1. 1) Tanatsugu, N., Sato, T., Naruo, Y., Kashiwagi, T., Mizutani, T., Monji, K. et al.: Development Study on ATREX Engine, Acta Astronautica, 41 (1997), pp. 851–862. 2. 2) Sato, T., Taguchi, H., Kobayashi, H., and Kojima, T.: Development study of Mach 6 Turbojet Engine with Air Precooling, J. British Interplanetary Society, 58 (2005), pp. 231–240. 3. 3) Taguchi, H., Harada, K., Kobayashi, H., Kojima, T., Hongoh, M., Masaki, D. et al.: Firing Test of a Hypersonic Turbojet Engine Installed on a Flight Test Vehicle, AIAA-Paper 2009-7311, 2009. 4. 4) Taguchi, H., Kobayashi, H., Kojima, T., Ueno, A., Imamura, S., Hongoh, M. et al.: Research on Hypersonic Aircraft Using Pre Cooled Turbojet Engines, Acta Astronautica, 73 (2012), pp. 164–172. 5. 5) Miwa, T., Taguchi, H., Matsuo, A., and Watanabe, K.: Evaluation of Heat Flux on HIMICO considering the Ablation of TPS, AIAA pe17-212,017.
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