Numerical Prediction of the Minimum Height of Roughness Strip for Artificial Transition on Swept Wings-Reference-Cited by-同舟云学术

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Numerical Prediction of the Minimum Height of Roughness Strip for Artificial Transition on Swept Wings

Published:2016-01-02 Issue: Volume: Page:
ISSN:
Container-title:54th AIAA Aerospace Sciences Meeting
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Author:

Tian Yongqiang¹,Zhang Zhengke¹,Zhai Qi¹,Qu Ke²

Affiliation:

1. Northwestern Polytechnical University

2. City University of New York

Publisher

American Institute of Aeronautics and Astronautics

Reference35 articles.

1. 1Fan, J. C., Wind Tunnel Experiment Handbook, Aviation Industry Press, Beijing, 2002, Chap. 6, pp.313-314. [in Chinese]

2. 4Cheng, H. M., Wind Tunnel Experiment Interference and Correction, National Defense Industrial Press, Modern AerodynamicsSeries, Beijing,2003, Chap.4, pp.292-299. [in Chinese]

3. 5Langtry, R. B. "A Correlation-based Transition Model Using Local Variables for Unstructured Parallelized CFD Codes," Ph.D. Thesis,Stuttgart University, Stuttgart, Germany, 2006.

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