基于马赫数分布可控曲面外/内锥形基准流场的前体/进气道一体化设计
李永洲, 张堃元
Integrated design of forebody and inlet based on external and internal conical basic flow field with controlled Mach number distribution surface
LI Yongzhou, ZHANG Kunyuan
航空学报
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2015, (1): 289
-301
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DOI: 10.7527/S1000-6893.2014.0263
CJA