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Comparisons: Category 4In this document, numerical solutions for acoustic pressure fields are compared with the analytical solution along three different lines: y = 15, y = 50, and x = 100. The document lists the computational resources used in the various submitted numerical solutions. These solutions are for a problem presented in the Fourth Computational Aeroacoustics (CAA) Workshop on Benchmark Problems. The solutions utilize frequency domain and time domain analysis.
Document ID
20040182274
Acquisition Source
Glenn Research Center
Document Type
Conference Paper
Authors
Philip J Morris (Pennsylvania State University State College, United States)
Anurag Agarwal (Pennsylvania State University State College, United States)
Date Acquired
August 22, 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
Portions of document may include copyright protected material.
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IDRelationTitle20040182258Collected WorksFourth Computational Aeroacoustics (CAA) Workshop on Benchmark Problems
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