Through experiments, effects of structural parameters of the nozzle on its performance are got to revise structural parameters.
通过实验，得到喷头的结构参数对喷头性能的影响，然后来修正喷头结构参数。
The experimental results verify that the feasible theory can be used to investigate the effects of structural parameters of hingeless rotor on aeroelastic stability.
试验证明该理论可行并能用于研究无铰旋翼结构参数对桨叶气弹稳定性的影响，也能用于直升机旋翼的型号设计。
The effects of structural parameters of Squeeze Film Damper (SFD), such as eccentricity, radial clearance and land length etc. on cavitation were investigated experimentally.
在实验的基础上，研究了挤压油膜阻尼器的结构参数诸如偏心率、油膜的径向间隙比和承载长度等对气穴现象的影响。
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