Comparison of High-Fidelity Computational Tools for Wing Design of a Distributed Electric Propulsion Aircraft-Reference-Cited by-同舟云学术

Comparison of High-Fidelity Computational Tools for Wing Design of a 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 Sally¹,Carter Melissa¹,Viken Jeffrey K.¹,Derlaga Joseph M.¹,Stoll Alex M.²

Affiliation:

1. NASA Langley Research Center

2. Joby Aviation

Publisher

American Institute of Aeronautics and Astronautics

Link

https://arc.aiaa.org/doi/pdf/10.2514/6.2017-3925

Reference21 articles.

1. ! Borer, N. K.; Derlaga, J. M.; Deere, K. A.; Carter, M. B.; Viken, S. A.; Patterson, M. D.; Litherland, B. L.; and Stoll, A. "Comparison of Aero-Propulsive Performance Predictions for Distributed Propulsion Configurations," AIAA 2017-0209.

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. ! Drela, M., and Youngren, H.: XROTOR Download Page, http://web.mit.edu/drela/Public/web/xrotor/, accessed 6 May 2014.

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