Numerical/Experimental Hybrid Study on Base Pressure and Cavity Pressure Corrections for Transonic Wind Tunnel Tests-Reference-Cited by-同舟云学术

Numerical/Experimental Hybrid Study on Base Pressure and Cavity Pressure Corrections for Transonic Wind Tunnel Tests

Published:2022 Issue:3 Volume:65 Page:116-122
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:

KAWASHIMA Hayato¹,KITAMURA Keiichi¹,NONAKA Satoshi²

Affiliation:

1. Graduate School of Engineering Science, Yokohama National University

2. Institute of Space and Astronautical Science, 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/65/3/65_T-21-21/_pdf

Reference22 articles.

1. 1) Kitamura, K., Nonaka, S., Kuzuu, K., Aono, J., Fujimoto, K., and Shima, E.: Numerical and Experimental Investigations of Epsilon Launch Vehicle Aerodynamics at Mach 1.5, J. Spacecr. Rockets, 50 (2013), pp. 896–916.

2. 2) Inatani, Y.: Study on a Reusable Rocket and Science Observation, Proceedings of the 3rd Space Science Symposium, 2003, pp. 377–380 (in Japanese).

3. 3) Forsythe, J. R., Hoffmann, K. A., Cummings, R. M., and Squires, K. D.: Detached-Eddy Simulation with Compressibility Corrections Applied to a Supersonic Axisymmetric Base Flow, J. Fluids Eng., 124 (2002), pp. 911–923.

4. 4) Tadakuma, K., Aso, S., Tani, Y., Mizoguchi, Y., and Okada, T.: An Experimental Study on Base Pressure Correction for Bluff-Base Bodies Using Magnetic Suspension and Balance System, J. Jpn. Soc. Aeronaut. Space Sci., 53 (2005), pp. 562–568 (in Japanese).

5. 5) Kitamura, K., Kuzuu, K., Irikado, T., and Nonaka, S.: Wind Tunnel Tests and Numerical Analyses on Aerodynamic Characteristics of Epsilon Launch Vehicle at Mach 0.7, Aerosp. Technol. Jpn. JSASS, 10 (2011), pp. 43–50 (in Japanese).

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