Dynamic Aeroelasticity of Wings with Tip Propeller by Using Navier–Stokes Equations
Author:
Affiliation:
1. NASA Ames Research Center, Moffett Field, California 94035
Funder
National Aeronautics and Space Administration
Publisher
American Institute of Aeronautics and Astronautics (AIAA)
Subject
Aerospace Engineering
Link
https://arc.aiaa.org/doi/am-pdf/10.2514/1.J058610
Reference26 articles.
1. Computational Analysis of a Wing Designed for the X-57 Distributed Electric Propulsion Aircraft
2. HeegJ.StanfordB.WiesemanC. D.MasseyS.MooreJ.TruaxR. A. “Status Report on Aeroelasticity in the Vehicle Development for X-57 Maxwell,” AIAA Applied Aerodynamics Conference, AIAA Paper 2018-3487, 2018. doi:10.2514/6.2018-3487
3. Whirl Flutter Stability and Its Influence on the Design of the Distributed Electric Propeller Aircraft X-57
4. Establishing Best Practices for X-57 Maxwell CFD Database Generation
5. Overview of NASA Electrified Aircraft Propulsion (EAP) Research for Large Subsonic Transports
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