建立了再入体再入大气层形成的尾迹的工程模型,并运用边界层理论求解二维等压湍流尾迹流动。
An engineering model for hypersonic reentry body trail is established in this paper, and a calculation is performed by using boundary layer theory.
建立了再入体再入大气层形成的尾迹的工程模型,并运用边界层理论求解二维等压湍流尾迹流动。
An engineering model for hypersonic reentry body trail is established in this paper, and a calculation is performed by using boundary layer theory.
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