Robust Design Optimization for Multiple Responses Using Response Surface Methodology and Taguchi Approach: Solid Rocket Motor Application
Author:
Affiliation:
1. The Scientific & Technological Research Council of Turkey - Defence Industries Research & Development Institute
Publisher
American Institute of Aeronautics and Astronautics
Link
http://arc.aiaa.org/doi/pdf/10.2514/6.2007-1977
Reference20 articles.
1. Reliability Analysis of a Solid Rocket Motor Based on Response Surface Method and Monte Carlo Simulation
2. Simultaneous Optimization of Several Response Variables
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3. Robust Structural Design Optimization of Flexible Backswept Wings;51st AIAA/ASME/ASCE/AHS/ASC Structures, Structural Dynamics, and Materials Conference<BR> 18th AIAA/ASME/AHS Adaptive Structures Conference<BR> 12th;2010-04-12
4. Reliability Based Design Optimization of A Solid Rocket Motor Using Surrogate Models;43rd AIAA/ASME/SAE/ASEE Joint Propulsion Conference & Exhibit;2007-07-08
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