Furthermore, a mathematical method calculating the aerodynamic disturbing force of transverse jet stream is presented.

给出了计算横向喷流气动干扰力的数学方法。

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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.

由于喷流方向与主流方向夹角较小，总压损失也较物理斜坡、横向喷流等混合增强方式小。

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Transverse bars may migrate down-stream relatively rapidly.

横向沙滩可以相当迅速地向下游移动。

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