Integrated Nacelle-Wing Shape Optimization for an Ultra-High Bypass Fanjet Installation on a Single-Aisle Transport Configuration
Author:
Affiliation:
1. NASA Ames Research Center
2. Science and Technology Corporation
3. NASA Langley Research Center
Publisher
American Institute of Aeronautics and Astronautics
Link
http://arc.aiaa.org/doi/pdf/10.2514/6.2013-543
Reference7 articles.
1. Trefftz-Plane Drag Minimization at Transonic Speeds
2. Campbell,RichardL."EfficientViscousDesignofRealsticAircraftConfigurations,"AIAA-98-2539,June1998.
3. Universal Parametric Geometry Representation Method
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