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1)  sting interference
尾支杆干扰
1.
Preliminary research on non-linear correction method of sting interference;
尾支杆干扰非线性修正方法的初步研究
2)  Eliminated sting interference
消除支杆干扰
3)  Wake interaction
尾流干扰
4)  Mating interfering
交尾干扰
5)  tail wave interference
尾波干扰
6)  tail sting
尾支杆
1.
During testing in supersonic wind tunnel,the model is supported in wind tunnel with a tail sting of balance at the base of model.
由于尾支杆的存在,使得模型底部流动发生畸变,引起底阻测量的不准确性。
2.
Presents the effect of tail sting and the angle of boat tail on the base pressure of a projectile in flight at supersonic velocities.
由于尾支杆的存在,使得模型底部流动发生畸变,引起底阻测量的不准确。
3.
Although the effect of tail sting on base-pressure ratio of a projectile in turbulent flow is smaller than that in laminar flow, experimental investigations have indicated that the relative base- pressure ratio of a projectile with tail sting increases as the relative turbulent boundarylayer thickness increases and reduces as the relatiye diameter increases in supersonic flow.
尽管在超声速湍流情况下,尾支杆对弹丸底部压力的影响没有层流情况下的影响大。
补充资料:摆放式干扰机(见通信干扰设备)


摆放式干扰机(见通信干扰设备)
hand-emplaced jammer

  baifongshi gQnraoii摆放式干扰机(hand一emplaeed jam;ner)见通信干扰设备。
  
说明:补充资料仅用于学习参考,请勿用于其它任何用途。
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