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Linear Unsteady CFD Analysis of the Cascade-Gust Interaction ProblemA linearised unsteady Navier-Stokes code, HYDLIN, is used to provide the results for the cascade-gust interaction test problem. The HYDLIN approach is based on linearistion of the unsteady flow about the cascade mean flow generated by the steady non-linear flow solution from the HYDRA CFD code. The test problem solutions for the workshop have been run using a multiblock quadrilateral mesh of around 48K nodes, using boundary conditions as defined in the test problem specification. The physical aspects of the cascade-gust interaction and the waves generated by the interaction are studied using the linear unsteady CFD results.
Document ID
20040182265
Acquisition Source
Glenn Research Center
Document Type
Conference Paper
Authors
John Coupland
(Rolls-Royce Ltd. London, United Kingdom)
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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