... d layer oil production rate ==> 分层产油量 d leading edge ==> 楔形进气边 d nozzle charateristic ==> 额定喷管特性 ...
基于16个网页-相关网页
Fixed d leading-edge wing slats 固定领先的机翼的缝翼
The unsteady flow field near the leading edge of an oscillating sweptback wing is obtained by using 3-D subsonic lifting surface theory.
本文应用三元亚音速升力面理论求出了后掠翼前缘附近的流场。
A 3-d wing is considered to have 100% leading-edge suction when the Oswald efficiency factor (e) exactly equals 1.0.
而对于三维机翼来说，当奥斯瓦德有效因数等于1.0时，可认为有100%的前缘吸力。
应用推荐