This paper introduces a wind tunnel experiment technique of side-back jet, aerodynamic interactions and predict method.
主要阐述了弹丸头部喷流风洞实验中的实验方法、动力干扰影响及预测方法。
The influence of clearance between the nozzles and the model of the surface pressure was used in the hybrid extended-range technique of the side back jet.
在风洞实验中采用纹影照相和压力分布相结合的实验方法,确定了侧后向喷流复合增程技术中喷嘴—模型之间间隙的大小对表面压力的影响。
The dog was then sent back to the U.S. on a private chartered jet.
然后,这只狗坐私人包机被送回了美国。
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