The present invention relates to an aircraft empennage surface and an aircraft, and more particularly to a configuration of an aircraft empennage surface having a single projection for improving airflow control without or without loss of resistance negligible.
本发明涉及飞行器尾翼表面和飞行器,并且更具体地涉及具有单个突出部的飞行器尾翼表面的构型,该突出部用于在没有阻力损失或阻力损失可忽略的情况下改善气流控制。
Aircraft empennage surface and aircraft
飞行器尾翼表面和飞行器
2025-05-20
Patent
Electronic Resource
Chinese
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