Off-design reynolds number effects for a supersonic transport

被引：0
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作者：
Owens, Lewis R. [1 ,2 ,3 ]
Wahls, Richard A. [1 ,3 ,4 ]
Rivers, S. Melissa [1 ,3 ,4 ]
机构：
[1] NASA Langley Research Center, Hampton, VA 23681-2199, United States
[2] Flow Physics and Control Branch, United States
[3] AIAA, United States
[4] Configuration Aerodynamics Branch, United States
来源：
Journal of Aircraft | 1600年 / 42卷 / 06期
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页码：1427 / 1441
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