Numerical Investigation of Powered High-Lift Model with Externally Blown Flap-Reference-Cited by-同舟云学术

Numerical Investigation of Powered High-Lift Model with Externally Blown Flap

Published:2017-07 Issue:4 Volume:54 Page:1539-1551
ISSN:0021-8669
Container-title:Journal of Aircraft
language:en
Short-container-title:Journal of Aircraft

Author:

Jie Li¹,Zhibin Gong¹,Heng Zhang¹,Jing Jin¹

Affiliation:

1. Northwestern Polytechnical University, 710072 Xi’an, People’s Republic of China

Funder

National Aerospace Science Foundation of China

National Key Basic Research Program of China

National Natural Science Foundation of China

Publisher

American Institute of Aeronautics and Astronautics (AIAA)

Subject

Aerospace Engineering

Link

https://arc.aiaa.org/doi/pdf/10.2514/1.C034270

Reference22 articles.

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3. CampbellJ. P.JohnsonJ. L. Jr. “Wind-Tunnel Investigation of an External Flow Jet-Augmented Slotted Flap Suitable for Application to Airplanes with Pod-Mounted Engines,” NASA TN-3898, 1956.

4. WashingtonH. P.GibbonsJ. T. “Analytical Study of Takeoff and Landing Performance for a Jet STOL Transport Configuration with Full-Span Externally Blown Triple-Slotted Flaps,” NASA TR D-7441, 1973.

5. Navier-Stokes analysis of a High Wing Transport high-lift configuration with externally blown flaps

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