anti icing system

基本解释

Numerical methods for determining the trajectories of the water droplets are studied for anti icing system design.
對水滴撞擊特性的數值計算方法進行了研究。
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Trajectories of water droplets were studied to provide information for anti icing system design of inlet of an engine.
針對某發動機進氣道的防冰系統設計，對進氣道的水滴撞擊特性進行了研究。
The results indicate that the structure of frontal anti icer affects anti icing effectiveness obviously for a hot air anti icing system, the double skin chord direction anti icer i.
飛機發動機防冰對飛行安全具有十分重要的意義，對於熱氣防冰系統，前緣防冰器的結搆型式對防冰的傚果影響很大。