Multidisciplinary Design Optimization of Supersonic Fighter Wing Using Response Surface Methodology
Author:
Publisher
American Institute of Aeronautics and Astronautics
Link
http://arc.aiaa.org/doi/pdf/10.2514/6.2002-5408
Reference13 articles.
1. 3Lollo, A., and Salas, M. D. "Optimum Transonic Airfoils Based on the Euler Equations," NASA CR201638.
2. Response Surface Method for Airfoil Design in Transonic Flow
3. Static and Dynamic Aeroelasticity of Advanced Aircraft Wings Carrying External Stores
4. Use of Analytical Flow Sensitivities in Static Aeroelasticity
5. Load and motion transfer algorithms for fluid/structure interaction problems with non-matching discrete interfaces: Momentum and energy conservation, optimal discretization and application to aeroelasticity
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1. Research on the Detail Design of Aircraft Wings;Applied Mechanics and Materials;2014-01
2. Coupled Aerodynamic/Structural Optimization of a Subsonic Transport Wing Using a Surrogate Model;Journal of Aircraft;2008-11
3. Multi-Objective and Multidisciplinary Design Optimization of Supersonic Fighter Wing;Journal of Aircraft;2006-05
4. Application of Collaborative Optimization Using Genetic Algorithm and Response Surface Method to an Aircraft Wing Design;Journal of Mechanical Science and Technology;2006-01
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