Computational Component Build-up for the X-57 Maxwell Distributed Electric Propulsion Aircraft-Reference-Cited by-同舟云学术

Computational Component Build-up for the X-57 Maxwell Distributed Electric Propulsion Aircraft

Published:2018-01-07 Issue: Volume: Page:
ISSN:
Container-title:2018 AIAA Aerospace Sciences Meeting
language:
Short-container-title:

Author:

Deere Karen A.¹,Viken Sally¹,Carter Melissa B.¹,Viken Jeffrey K.¹,Cox David E.¹,Wiese Michael R.²,Farr Norma L.²

Affiliation:

1. NASA Langley Research Center

2. Craig Technologies, Inc.

Publisher

American Institute of Aeronautics and Astronautics

Link

https://arc.aiaa.org/doi/pdf/10.2514/6.2018-1275

Reference26 articles.

1. 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.

2. Tetrahedral Unstructured Navier-Stokes Method for Turbulent Flows

3. CFD Computations for a Generic High-Lift Configuration Using TetrUSS

Cited by 11 articles. 订阅此论文施引文献订阅此论文施引文献，注册后可以免费订阅5篇论文的施引文献，订阅后可以查看论文全部施引文献

1. Quasi-three-dimensional high-lift wing design approach considering three-dimensional effects of slipstream for distributed electric propulsion aircraft;Chinese Journal of Aeronautics;2024-06

2. Two Aerodynamic Mid-Fidelity Approaches on a Distributed Propulsion Wing;Journal of Aircraft;2023-12-18

3. Performance analysis and flow mechanism of channel wing considering propeller slipstream;Chinese Journal of Aeronautics;2023-11

4. Conceptual Design and Optimization of Distributed Electric Propulsion General Aviation Aircraft;Aerospace;2023-04-22

5. Energy efficient design and implementation of electric machines in air transport propulsion system;Applied Energy;2022-09