An Integral Boundary Layer Direct Method Applied to 2D Transonic Small-Disturbance Equations
Author:
Affiliation:
1. University of Washington, Seattle
2. MORI Associates, Inc.
3. NASA Ames Research Center
Publisher
American Institute of Aeronautics and Astronautics
Link
http://arc.aiaa.org/doi/pdf/10.2514/6.2016-3568
Reference11 articles.
1. Thirty years of development and application of CFD at Boeing Commercial Airplanes, Seattle
2. Aeroelastic Modeling of Elastically Shaped Aircraft Concept via Wing Shaping Control for Drag Reduction
3. Elastically Shaped Wing Optimization and Aircraft Concept for Improved Cruise Efficiency
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