The paper investigates the problem on vortex generator control boundary layer's separation of supercritical airfoil and wing for body configuration wing.
本文研究涡流发生器控制超临界翼型和翼身组合体机翼的附面层分离问题。
The invention discloses a reinforced heat transfer element of a truncated cylindrical surface wing type vortex generator, belonging to the field of heat transfer parts of heat exchanger.
本发明公开了属于换热器传热零部件领域的一种斜截柱面翼式涡发生器强化传热元件。
With TUSA, the vortex generator which from the past in the wing and the racing car of the airplane is installed for preventing the air current exfoliation it applied then.
与TUSA，从过去在翼和飞机赛车被安装为防止气流剥落的漩涡发电器它然后申请了。
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