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(dòng)機(jī)葉片的設(shè)計(jì)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(xiàng)目設(shè)計(jì)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(shí)驗(yàn)的方法模擬研究了渦輪葉片尾緣出流對(duì)帶叉排擾流柱陣列的內(nèi)冷通道的對(duì)流換熱特性的影響。