Distributed Propulsion Aircraft with Aeroelastic Wing Shaping Control for Improved Aerodynamic Efficiency
Author:
Affiliation:
1. NASA Ames Research Center, Moffett Field, California 94035
2. Universities Space Research Association, Moffett Field, California 94035
Publisher
American Institute of Aeronautics and Astronautics (AIAA)
Subject
Aerospace Engineering
Link
https://arc.aiaa.org/doi/pdf/10.2514/1.C034448
Reference32 articles.
1. Turboelectric Distributed Propulsion Engine Cycle Analysis for Hybrid-Wing-Body Aircraft
2. The Potential and Challenge of TurboElectric Propulsion for Subsonic Transport Aircraft
3. Preliminary Experimental Assessment of the Boundary Layer Ingestion Benefit for the D8 Aircraft
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