inner passage

基本解釋

The cooling technique of the blade inner passage plays a significant role in the design of blades for gas turbine.
葉片內(nèi)部通道冷卻技術(shù)在航空發(fā)動機葉片的設(shè)計中占有重要的位置。
An inner air passage is created introducing monsoon from the outer openings of the whole building in order to provide natural ventilation.
為了讓建筑自然通風(fēng)，項目設(shè)計了一條內(nèi)部空氣通道，將建筑室外的季風(fēng)導(dǎo)入到內(nèi)部。
An experimental research was conducted to simulate the effect of trailing edge ejection of turbine blades on heat transfer of the inner cooling passage with staggered pin fin array.
本文用實驗的方法模擬研究了渦輪葉片尾緣出流對帶叉排擾流柱陣列的內(nèi)冷通道的對流換熱特性的影響。