Integrated Transition Prediction: A Case Study in Supersonic Laminar Flow Control
Integrated Transition Prediction: A Case Study in Supersonic Laminar Flow Control
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DOI：
10.2514/6.2003-973
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发表时间：
2003-01
期刊：
影响因子：
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通讯作者：
Meelan Choudhari;C. Chang;C. Streett;P. Balakumar
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文献类型：
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作者：
Meelan Choudhari;C. Chang;C. Streett;P. Balakumar
航空航天技术专家，计算建模与仿真分支，高级会员AIAA航空航天技术专家，计算建模与仿真分支。larc.nasa.gov * 航空航天技术专家，流动物理和控制分支，高级会员AIAA版权所有© 2003年由美国航空航天研究所，公司。在美国，根据美国法典第17条，没有版权主张。美国政府拥有免版税许可证，可出于政府目的行使本文所述版权下的所有权利。版权所有者保留所有其他权利。摘要
† Aerospace Technologist, Computational Modeling and Simulation Branch, Senior Member AIAA Email: m.m.choudhari@larc.nasa.gov †† Aerospace Technologist, Computational Modeling and Simulation Branch, Senior Member AIAA ††† Aerospace Technologist, Computational Modeling and Simulation Branch. * Aerospace Technologist, Flow Physics and Control Branch, Senior Member AIAA Copyright © 2003 by the American Institute of Aeronautics and Astronautics, Inc. No copyright is asserted in the United States under Title 17, U.S. Code. The U.S. Government has a royalty-free license to exercise all rights under the copyright claimed herein for Governmental Purposes. All other rights are reserved by the copyright owner. Abstract