Fl low-speed tests of a high-lift system on a highly-swept wing

G. OUTTIER; G. TOURON

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Fl low-speed tests of a high-lift system on a highly-swept wing

机译：在高掠过的机翼上进行高升力系统的Fl低速测试

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The main objective of the French Civil Aviation DTP related to a Highly-Swept Wing High-Lift System (HFF), was to achieve the design of high-lift devices for high cruise Mach number aircraft, which provides acceptable performance at low-speeds for take-off and landing. The design was based on a methodology that combined experimental data from the ONERA Fl wind tunnel with CFD calculations. The project was jointly led by Dassault Aviation and ONERA's Applied Aerodynamics Department (DAAP).

机译：法国民航DTP的主要目标是与高掠过的机翼高升空系统（HFF）相关，以实现用于高巡航马赫数飞机的高升力设备的设计，从而在低速飞行时提供可接受的性能。起飞和着陆。该设计基于将ONERA Fl风洞的实验数据与CFD计算相结合的方法。该项目由达索航空和ONERA的应用空气动力学部门（DAAP）共同领导。

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《ONERA Scientific and Technical Activities》 |2006年第2006期|p.18-19|共2页
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G. OUTTIER; G. TOURON;
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Fl low-speed tests of a high-lift system on a highly-swept wing

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