Numerical Simulation of Powered High-Lift Flow

Zhi Bin Gong; Jie Li; Bin Tian

doi:10.4028/www.scientific.net/AMR.1016.501

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HomeAdvanced Materials ResearchAdvanced Materials Research Vol. 1016Numerical Simulation of Powered High-Lift Flow

Numerical Simulation of Powered High-Lift Flow

Abstract:

To achieve short-take-off-and-landing (STOL) performance, numerous airframe/propulsion integration (API) technologies have been developed for military and commercial transports. Powered lift technology refers to a concept of utilizing the propulsion exhaust flows to increase lift through an increase in wing circulation []. Over the past seventy years, various concepts have been explored to accomplish this goal. From the point of view of technical characteristics, powered lift concepts can be sorted into three groups: a circulation control wing, blown flaps, and jet wing. Most of other concepts are slight deviations of these three.

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Periodical:

Advanced Materials Research (Volume 1016)

Pages:

501-505

DOI:

https://doi.org/10.4028/www.scientific.net/AMR.1016.501

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Online since:

August 2014

Authors:

Zhi Bin Gong*, Jie Li, Bin Tian

Keywords:

Aerodynamic Properties, Externally Blown Flap, RANS Method, Structured Grid

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* - Corresponding Author

References

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