Sensitivity Analysis and Optimization of Delta Wing Design Parameters using CFD-Based Response Surface Method

Sensitivity Analysis and Optimization of Delta Wing Design Parameters using CFD-Based Response Surface Method

This paper explores the effect of design variables on the objective functions of clipped delta wing with a modified double-wedge airfoil section based on parametric analysis and CFD-based optimization using response surface method. This type of wing is used in air-launch-to-orbit vehicles. The thick...

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Bibliographic Details
Main Authors: M. Aelaei, S. Karimian, F. Ommi
Format: Article
Language:English
Published: Isfahan University of Technology 2019-01-01
Series:Journal of Applied Fluid Mechanics
Subjects:
Delta wing; Air launch-to-orbit vehicle
aerodynamic efficiency; NSGA-II Optimization; Response Surface Methodology.
Online Access:http://jafmonline.net/JournalArchive/download?file_ID=50095&issue_ID=1003

Internet

http://jafmonline.net/JournalArchive/download?file_ID=50095&issue_ID=1003

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