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Category 3, Problem 1: Comparison of Solutions, Wang et alCharts are displayed to show comparison of RMS pressure on airfoil surface, comparison of acoustic intensity on circle R = 1C, circle R = 4C, and circle R = 2C.
Document ID
20040182269
Acquisition Source
Glenn Research Center
Document Type
Conference Paper
Authors
James R Scott (Glenn Research Center Cleveland, United States)
Date Acquired
September 7, 2013
Publication Date
September 1, 2004
Publication Information
Publication: Fourth Computational Aeroacoustics (CAA) Workshop on Benchmark Problems
Publisher: National Aeronautics and Space Administration
Subject Category
Acoustics
Report/Patent Number
NASA/CP-2004-212954
Meeting Information
Meeting: 4th Computational Aeroacoustics (CAA) Workshop on Benchmark Problems
Location: Brook Park, OH
Country: US
Start Date: October 20, 2003
End Date: October 22, 2003
Sponsors: Ohio Aerospace Institute, Glenn Research Center
Distribution Limits
Public
Copyright
Work of the US Gov. Public Use Permitted.

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