An airfoil having a leading edge and a trailing edge and a suction surface and a pressure surface is disclosed, the suction surface including an ejector slit toward the leading edge. At least one additional slat may be provided toward the trailing edge. The airfoil may be configured for an aircraft. A method of operating an aircraft using such an airfoil is also disclosed.
公开了一种具有前缘和后缘以及吸力面和压力面的翼型,吸力面包括朝向前缘的喷射器翼缝。可设有朝向后缘的至少一个附加翼缝。翼型可构造用于飞机。还公开了一种使用这种翼型操作飞机的方法。
Airfoil with enhanced lift
具有增强升力的翼型
2023-09-01
Patent
Electronic Resource
Chinese
IPC: | B64C AEROPLANES , Flugzeuge |