Investigation of Model Wake Blockage Effects at High Angles of Attack in Low-Speed Wind Tunnel-Reference-Cited by-同舟云学术

Investigation of Model Wake Blockage Effects at High Angles of Attack in Low-Speed Wind Tunnel

Published:2008 Issue:171 Volume:51 Page:37-42
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:

SHYU Lih-Shyng,CHUANG Shu-Hao

Publisher

Japan Society for Aeronautical and Space Sciences

Subject

Space and Planetary Science,Aerospace Engineering

Link

https://www.jstage.jst.go.jp/article/tjsass/51/171/51_171_37/_pdf

Reference16 articles.

1. 1) Lan, C. E., Li, J., Yau, W. and Brandon, J. M.: Longitudinal and Lateral-Directional Coupling Effects on Nonlinear Unsteady Aerodynamic Modeling from Flight Data, AIAA Paper 2002-4804, 2002.

2. 2) Rae, W. H. and Pope, A.: Low Speed Wind Tunnel Testing, 2nd ed., John Wiley & Sons, Inc., USA, 1984, pp. 344–441.

3. 3) Attlesey, R. E.: Airflow Calibration and Model Blockage Correction, GDLST-ZA-228, General Dynamics, Convair Division, 1985.

4. 4) Goldstein, S. and Young, A. D.: The Linear Perturbation Theory of Compressible Flow, with Applications to Wind Tunnel Interference, ARC R&M 1909, 1943.

5. 5) Glauert, H.: Wind Tunnel Interference on Wings, Bodies and Airscrews, ARC R&M 1566, 1933.

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