Design of the Cruise and Flap Airfoil for the X-57 Maxwell Distributed Electric Propulsion Aircraft-Reference-Cited by-同舟云学术

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Design of the Cruise and Flap Airfoil for the X-57 Maxwell Distributed Electric Propulsion Aircraft

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

Author:

Viken Jeffrey K.¹,Viken Sally¹,Deere Karen A.¹,Carter Melissa¹

Affiliation:

1. NASA Langley Research Center

Publisher

American Institute of Aeronautics and Astronautics

Link

https://arc.aiaa.org/doi/pdf/10.2514/6.2017-3922

Reference11 articles.

1. 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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