Drag Reduction of a Near-Sonic Airplane by Using Computational Fluid Dynamics
Author:
Affiliation:
1. Tohoku University, Sendai 980-8579, Japan
Publisher
American Institute of Aeronautics and Astronautics (AIAA)
Subject
Aerospace Engineering
Link
http://arc.aiaa.org/doi/pdf/10.2514/1.15059
Reference18 articles.
1. Wing design for supersonic transports using integral equation method
2. The aerodynamic design of the wing-fuselage for a near-sonic transport
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1. Aerodynamic shape optimization of a near-sonic passenger plane using computational fluid dynamics;Proceedings of the Institution of Mechanical Engineers, Part G: Journal of Aerospace Engineering;2008-07-01
2. Aerodynamic Optimization of Essentially Three-Dimensional Shapes for Wing-Body Fairing;AIAA Journal;2008-07
3. Wing Shape Optimization of a Near-Sonic Passenger Plane;25th AIAA Applied Aerodynamics Conference;2007-06-15
4. Current Capability of Unstructured-Grid CFD and a Consideration for the Next Step;High Performance Computing on Vector Systems 2007
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