Supersonic Ejector-Driving System under Low Pressure: A Performance Evaluation-Reference-Cited by-同舟云学术

Supersonic Ejector-Driving System under Low Pressure: A Performance Evaluation

Published:2021 Issue:3 Volume:64 Page:156-164
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:

ANYOJI Masayuki¹,NUMATA Daiju²,NAGAI Hiroki³,ASAI Keisuke⁴

Affiliation:

1. Interdisciplinary Graduate School of Engineering Science, Kyushu University

2. Department of Aeronautics and Astronautics, Tokai University

3. Institute of Fluid Science, Tohoku University

4. Department of Aerospace Engineering, Tohoku University

Publisher

Japan Society for Aeronautical and Space Sciences

Subject

Space and Planetary Science,Aerospace Engineering

Link

https://www.jstage.jst.go.jp/article/tjsass/64/3/64_T-20-16/_pdf

Reference16 articles.

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3. 3) Nagai, H. and Mars Airplane Working Group: Aerodynamic Challenge to Realize Mars Airplane, Proceeding of 30th International Symposium on Space Technology and Science, Kobe, Japan, 2015-k-47, 2015.

4. 4) Fujita, K., Nagai, H., and Asai, K.: Conceptual Design of a Miniature, Propeller-Driven Airplane for Mars, AIAA Paper 2012-0847, 2012.

5. 5) Anyoji, M., Nose, K., Ida, S., Numata, D., Nagai, H., and Asai, K.: Development of a Low-Density Wind Tunnel for Simulating Martian Atmospheric Flight, Trans. JSASS Aerospace Technology Japan, 9 (2011), pp. 21–27.

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