Experimental Measurements of Starting Loads and Model Behaviors in the Indraft Supersonic Wind Tunnel

Author:

MINATO Ryojiro,MIZOBATA Kazuhide,KUWATA Komei

Publisher

Japan Society for Aeronautical and Space Sciences

Subject

Space and Planetary Science,Aerospace Engineering

Reference8 articles.

1. 1) Pope, A. and Goin, K. L.: High Speed Wind Tunnel Testing, Robert, E., ed., Krieger Publishing Company, Malabar, Florida, 1965, pp. 365–369.

2. 2) Iijima, H., Watanabe, M., Kanda, H., Sato, M., Nagai, S. and Suzuki, N.: Effects of Several Parameters on Starting/Stopping Loads in Supersonic Wind Tunnels, JAXA Research and Development Report, JAXA-RR-05-048, 2006 (in Japanese).

3. 3) Maydew, R. C.: Compilation and Correlation of Model Starting Loads from Several Supersonic Tunnels, Sandia Corporation-4691 (RR), 1962.

4. 4) Crane, J. F. W. and Woodley, J. G.: The 7in.×7in. Hypersonic Wind Tunnel at R.A.E. Farnborough, Part IV—Measurements of Diffuser Performance, Blockage, Starting Loads and Humidity, Aeronautical Research Council Current Papers, No. 663 1963.

5. 5) Irikado, T., Sato, K. and Fujii, K.: Transient Loads and Flow Structures in the ISAS Supersonic Wind Tunnel, Proceedings of the 38th Fluid Dynamics Conference, Muroran, 2006, pp. 259–262 (in Japanese).

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