Improvement of a sensitivity-adjustable three component force balance and its application to supersonic wind tunnel testing
Author:
Affiliation:
1. Department of Mechanical and Aerospace Engineering, Tottori University
2. Institute of Fluid Science, Tohoku University
Publisher
Japan Society of Mechanical Engineers
Subject
Fluid Flow and Transfer Processes,Mechanical Engineering
Link
https://www.jstage.jst.go.jp/article/jfst/9/5/9_2014jfst0068/_pdf
Reference10 articles.
1. Kato, S., Kawazoe, H., Okano, M. and Matsuno, T., Aerodynamic characteristics of nonslender flexible delta wing in pitching motion, Proceedings of the 25th International Symposium on Space Technology and Science (2006), pp.714-719.
2. Kawazoe, H., Yorikane, T. and Matsumoto, M., Experimental study on dynamic characteristics of delta wing in pitching motion, 30th AIAA Fluid Dynamics Conference (1999), AIAA-99-3520.
3. Kawazoe, H. and Morita, S., Altitude effects of rolling delta wing on the dynamics characteristics, 33rd AIAA Fluid Dynamics Conference (2003), AIAA-2003-3471.
4. Kawazoe, H. and Kato, S., Effects of leading edge separation vortex of flexible structure delta wing on its aerodynamic characteristics, JSME International Journal Series B, Vol.49, No.4 (2006), pp.1049-1054.
5. Liepmann, H. W. and Roshko, A., Elements of gasdynamics, John Wiley & Sons, Inc. (1965), p.59.
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