进口流道中的气弹和气柱导致了阳极传质恶化。
Gas slugs and gas columns in the inlet channels lead to block of mass transfer in the anode.
以动力学模型和气动模型相匹配为原则，建立了后掠桨尖旋翼的细致气弹模型。
A refined aeroelastic model of a helicopter rotor blade with swept tips is established based on model matching.
经与有限元计算结果比较后可知，所识别的全桥气弹模型固有频率和振型结果令人满意。
The identified natural frequencies and mode shapes are found satisfying via a comparison with those obtained by finite element computation.
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