afterbody

基本解釋

The flow over the Geimini afterbody is separated.
雙子星座后體處于分離狀態(tài)。
The more the afterbody flatness, the more the pressure drag.
后體越扁平，其壓差阻力系數(shù)越大；
The research was made on the afterbody flow field of civil aircraft.
本文運用計算與實驗相結合的研究方法對民機機身后體流場進行了研究。
The friction drag coefficient increases with increasing afterbody fineness ratio and decreasing Reynolds Number.
后體摩擦阻力系數(shù)分別隨后體的長細比的增加和雷諾數(shù)的減小而增加；
The vectoring jet effects are not only limited on the afterbody near the nozzle, but also on the forebody far away from the nozzles.
而噴流對附著流動和穩(wěn)定旋渦流動的干擾效應最弱且集中于噴口附近。