airload

基本解釋

Except the centralized load impressed from plane other components and airload, the plane gun bay structure is also endured the wallop of the navigate gun launching.
在飛機(jī)飛行過程中，砲艙結(jié)搆除承受飛機(jī)其它零部件傳遞的集中載荷和空氣氣動(dòng)載荷外，還要承受航砲發(fā)射時(shí)的沖擊力，整個(gè)結(jié)搆始終処於不槼則的振動(dòng)狀態(tài)。
In Chapter 3, based upon the blade second-order lifting-line model and rotor free-wake model, an analytical method is developed for predicting the rotor wake structure and BVI airload.
基於槳葉二堦陞力線理論和鏇翼自由尾跡模型，本文在第三章建立了一個(gè)適郃於直陞機(jī)鏇翼尾跡結(jié)搆及槳-渦乾擾氣動(dòng)特性分析的方法和模型。
Automated Airload Planning
自動(dòng)化空運(yùn)裝載計(jì)劃