Aerodynamic Characteristics of Busemann Biplane by Wake Measurements in Low-Speed Wind Tunnel-Reference-Cited by-同舟云学术

Aerodynamic Characteristics of Busemann Biplane by Wake Measurements in Low-Speed Wind Tunnel

Published:2021 Issue:5 Volume:64 Page:258-266
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:

KASHITANI Masashi¹,NGUYEN Thai Duong²,KUSUNOSE Kazuhiro³,TAGUCHI Masato¹,TAKITA Yoshihiro⁴

Affiliation:

1. Department of Aerospace Engineering, National Defense Academy

2. Graduate School of Science and Engineering, National Defense Academy

3. Formerly, Japan Aerospace Exploration Agency

4. Department of Information Engineering, National Defense Academy

Publisher

Japan Society for Aeronautical and Space Sciences

Subject

Space and Planetary Science,Aerospace Engineering

Link

https://www.jstage.jst.go.jp/article/tjsass/64/5/64_T-20-37/_pdf

Reference25 articles.

1. 1) Kusunose, K.: Aerodynamic Design of Supersonic Biplane, The 21st COE Program Lecture Series, Vol. 5, Tohoku University Press, Sendai, 2007, pp. 7–9.

2. 2) Liepmann, H. W. and Roshko, A.: Elements of Gas Dynamics, John Wiley & Sons, New York, 1957, pp. 107–123.

3. 3) Kusunose, K., Matsushima, K., Goto, Y., Yonezawa, M., Maruyama, D., and Nakano, T.: A Fundamental Study for the Development of Boomless Supersonic Transport Aircraft, AIAA Paper 2006-0654, 2006.

4. 4) Kusunose, K., Matsushima, K., Goto, M., Maruyama, D., Yamashita, H., and Yonezawa, M.: A Study in the Supersonic Biplane Utilizing Its Shock Wave Cancellation Effect, J. JSASS, 55, 636 (2007), pp. 1–7 (in Japanese).

5. 5) Maruyama, D., Matsushima, K., and Nakahashi, K.: Aerodynamic Analyses of Airfoil Configurations of Biplane Type Supersonic Transport, Trans. JSME, Part B, 72, 9 (2006), pp. 2132–2139 (in Japanese).

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