Boundary-layer transition of advanced fighter wings at high-speed cruise conditions
Author:
Funder
National Natural Science Foundation of China
Publisher
Elsevier BV
Subject
Mechanical Engineering,Aerospace Engineering
Reference34 articles.
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5. Jing ZR, Huang ZF. Instability analysis and drag coefficient prediction on a swept RAE2822 wing with constant lift coefficient. Chinese Journal of Aeronautics 2017; 30(3):964–75.
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