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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
Scott, James R. (NASA Glenn Research Center Cleveland, OH, United States)
Date Acquired
September 7, 2013
Publication Date
September 1, 2004
Publication Information
Publication: Fourth Computational Aeroacoustics (CAA) Workshop on Benchmark Problems
Subject Category
Acoustics
Distribution Limits
Public
Copyright
Work of the US Gov. Public Use Permitted.

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