Computational Analysis of Powered Lift Augmentation for the LEAPTech Distributed Electric Propulsion Wing-Reference-Cited by-同舟云学术

Computational Analysis of Powered Lift Augmentation for the LEAPTech Distributed Electric Propulsion Wing

Published:2017-06-02 Issue: Volume: Page:
ISSN:
Container-title:35th AIAA Applied Aerodynamics Conference
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Author:

Deere Karen A.¹,Viken Sally¹,Carter Melissa¹,Viken Jeffrey K.¹,Wiese Michael²,Farr Norma²

Affiliation:

1. NASA Langley Research Center

2. Craig Technologies

Publisher

American Institute of Aeronautics and Astronautics

Link

https://arc.aiaa.org/doi/pdf/10.2514/6.2017-3921

Reference13 articles.

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3. Wentz, W.H., Jr.; and Setharam, H. C. "Development of a Fowler Flap System for a High Performance General Aviation Airfoil," NASA Contractor Report CR-2443, December 1974.

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