Three-dimensional numerical simulation of an array of subsonic counter-flow jets issuing from a wing leading edge exposed to hypersonic aerodynamic heating
Three-dimensional numerical simulation of an array of subsonic counter-flow jets issuing from a wing leading edge exposed to hypersonic aerodynamic heating
复制标题
从暴露于高超声速气动加热的机翼前缘喷出的亚音速逆流射流阵列的三维数值模拟
DOI：
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发表时间：
2019
期刊：
影响因子：
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通讯作者：
Taku Ohwada
中科院分区：
文献类型：
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作者：
島田丈慶;大和田拓;Taku Ohwada
