Transonic Wind Tunnel Simulation with Porous Wall and Support Devices-Reference-Cited by-同舟云学术

Transonic Wind Tunnel Simulation with Porous Wall and Support Devices

Published:2010-06-28 Issue: Volume: Page:
ISSN:
Container-title:27th AIAA Aerodynamic Measurement Technology and Ground Testing Conference
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Author:

Hashimoto Atsushi¹,Aoyama Takashi¹,Kohzai Masataka¹,Yamamoto Kazuomi¹

Affiliation:

1. Japan Aerospace Exploration Agency (JAXA)

Publisher

American Institute of Aeronautics and Astronautics

Link

http://arc.aiaa.org/doi/pdf/10.2514/6.2010-4201

Reference16 articles.

1. 1Ueno,M.,Sudani,N."FlowAngularityMeasurementof2m2mTransonicWindTunnel,"AIAApaper2008-849,2008.

2. 2Kohzai, M., Ueno, M., Shiohara, T., Sudani, N. "Calibration of the test section Mach number in the JAXA 2m2m TransonicWindTunnel," AIAA2008-848,2008.

3. 3Kohzai, M., Shiohara, T., Ueno, M., Komatsu, Y., Karasawa, T., Koike, A., Sudani, N., Gahana, Y., Ikeda, M., Watanabe, A., Haraguchi, T., Nakagawa, M., Udagawa, D. "Thermal Zero Shift Correction of Strain-Gage Balance Output in the JAXA 2m2mTransonicWind Tunnel,"JAXAResearchand Development Report, JAXA-RR-07-034E, 2008.

4. 4Kohzai, M., Sudani, N., Yamamoto, K., Ueno, M. "Experimental and Numerical Studies of Support Interference in the JAXA2m2mTransonicWindTunnel," AIAApaper2010-4200,2010.

5. 5Mokry, M. "Subsonic Wall Interference Corrections for Finite-Length Test Sections Using Boundary Pressure Measurements,"Proceedings oftheFluid Dynamics Panel Specialists'Meeting,1982,pp.10.1-10.5, AGARD CP-335.

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