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Focused Assessment of State-of-the-Art CFD Capabilities for Prediction of Subsonic Fixed Wing Aircraft AerodynamicsSeveral recent workshops and studies are used to make an assessment of the current status of CFD for subsonic fixed wing aerodynamics. Uncertainty quantification plays a significant role in the assessment, so terms associated with verification and validation are given and some methodology and research areas are highlighted. For high-subsonic-speed cruise through buffet onset, the series of drag prediction workshops and NASA/Boeing buffet onset studies are described. For low-speed flow control for high lift, a circulation control workshop and a synthetic jet flow control workshop are described. Along with a few specific recommendations, gaps and needs identified through the workshops and studies are used to develop a list of broad recommendations to improve CFD capabilities and processes for this discipline in the future.
Document ID
20080023857
Acquisition Source
Langley Research Center
Document Type
Conference Paper
Authors
Rumsey, Christopher L.
(NASA Langley Research Center Hampton, VA, United States)
Wahls, Richard A.
(NASA Langley Research Center Hampton, VA, United States)
Date Acquired
August 24, 2013
Publication Date
June 1, 2008
Subject Category
Aeronautics (General)
Report/Patent Number
L-19484
NASA/TM-2008-215318
Report Number: L-19484
Report Number: NASA/TM-2008-215318
Funding Number(s)
WBS: WBS 561581.02.08.07.20.02
Distribution Limits
Public
Copyright
Work of the US Gov. Public Use Permitted.
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