Computational Analysis of a Wing Designed for the X-57 Distributed Electric Propulsion Aircraft-Reference-Cited by-同舟云学术

Computational Analysis of a Wing Designed for the X-57 Distributed Electric Propulsion Aircraft

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 Jeffrey K.¹,Viken Sally¹,Carter Melissa B.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/10.2514/6.2017-3923

Reference20 articles.

1. "New Aviation Horizons Initiative and Complementary Investments," NP-2016-06-2167-HQ, NASA Headquarters.

2. Biedron, R. T., Carlson, J. R.; Derlaga, J. M.; Gnoffo, P. A.; Hammond, D. P.; Jones, W. T.; Kleb, B.; Lee-Rausch, E. M.; Nielsen, E. J.; Park, M. A.; Rumsey, C. L.; Thomas, J. L.; and Wood, W. A. "FUN3D Manual: 13.0," NASA TM-2016-219330.

3. Tetrahedral Unstructured Navier-Stokes Method for Turbulent Flows

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