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Profile Optimization Method for Robust Airfoil Shape Optimization in Viscous FlowSimulation results obtained by using FUN2D for robust airfoil shape optimization in transonic viscous flow are included to show the potential of the profile optimization method for generating fairly smooth optimal airfoils with no off-design performance degradation.
Document ID
20030053190
Acquisition Source
Langley Research Center
Document Type
Technical Memorandum (TM)
Authors
Li, Wu (NASA Langley Research Center Hampton, VA, United States)
Date Acquired
September 7, 2013
Publication Date
May 1, 2003
Subject Category
Aerodynamics
Report/Patent Number
L-18283
NAS 1.15:212408
NASA/TM-2003-212408
Report Number: L-18283
Report Number: NAS 1.15:212408
Report Number: NASA/TM-2003-212408
Funding Number(s)
WORK_UNIT: WU 762-20-61-01
Distribution Limits
Public
Copyright
Work of the US Gov. Public Use Permitted.

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