NASA NTRS · 20040182269
Category 3, Problem 1: Comparison of Solutions, Wang et al
Abstract
Charts 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.
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Scott, James R.. 2004-09-01. Category 3, Problem 1: Comparison of Solutions, Wang et al. https://ntrs.nasa.gov/citations/20040182269
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