• But total pressure loss increases with the increasing of the velocity difference accompanied with the increase of the density and the static temperature ratio.

    速度密度比增大而增大时损失随之增大

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  • Due to the smaller Angle of injection, the ratio of total pressure loss of aerodynamic ramp is less than the physical ramp and transverse injection stream.

    由于方向与主流方向夹角较小损失物理斜坡横向喷流等混合增强方式小。

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  • At the end of the annular passage, shock wave occurs when the relative lift is less than 6% and the pressure ratio is less than 0.7, which causes a greater total pressure loss.

    相对升程小于6%、小于0.7环形通道末端产生激波,激波带来较大的损失

    youdao

  • At the end of the annular passage, shock wave occurs when the relative lift is less than 6% and the pressure ratio is less than 0.7, which causes a greater total pressure loss.

    相对升程小于6%、小于0.7环形通道末端产生激波,激波带来较大的损失

    youdao

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