Aircraft Design with Active Load Alleviation and Natural Laminar Flow
Author:
Affiliation:
1. Department of Aeronautics and Astronautics, Stanford University, Stanford, California 94305
Publisher
American Institute of Aeronautics and Astronautics (AIAA)
Subject
Aerospace Engineering
Link
http://arc.aiaa.org/doi/pdf/10.2514/1.C032402
Reference57 articles.
1. MartyB.ChristopherD. “Subsonic Ultra Green Aircraft Research: Phase I Final Report,” NASA Technical Rept. NASA/CR-2011-216847, 2011.
2. Improving the Airplane Efficiency by Use of Wing Maneuver Load Alleviation
3. Analysis for the Application of Hybrid Laminar Flow Control to a Long-Range Subsonic Transport Aircraft
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