NASA Logo

NTRS

NTRS - NASA Technical Reports Server

Back to Results
Comparison of Analytical and CAA Solutions: Single Airfoil Gust ResponseThe purpose of this problem is to test the ability of a computational fluid dynamics/computational aeroacoustics code to accurately predict the unsteady aerodynamic and aeroacoustic response of a single airfoil to a two-dimensional, periodic vortical gust.
Document ID
20010061421
Document Type
Conference Paper
Authors
Scott, James R.
(NASA Glenn Research Center Cleveland, OH United States)
Date Acquired
August 20, 2013
Publication Date
August 1, 2000
Publication Information
Publication: Third Computational Aeroacoustics (CAA) Workshop on Benchmark Problems
Subject Category
Acoustics
Distribution Limits
Public
Copyright
Work of the US Gov. Public Use Permitted.

Related Records

IDRelationTitle20010061385Analytic PrimaryThird Computational Aeroacoustics (CAA) Workshop on Benchmark Problems
Document Inquiry
No Preview Available