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Pressure wave propagation studies for oscillating cascadesThe unsteady flow field around an oscillating cascade of flat plates is studied using a time marching Euler code. Exact solutions based on linear theory serve as model problems to study pressure wave propagation in the numerical solution. The importance of using proper unsteady boundary conditions, grid resolution, and time step is demonstrated. Results show that an approximate non-reflecting boundary condition based on linear theory does a good job of minimizing reflections from the inflow and outflow boundaries and allows the placement of the boundaries to be closer than cases using reflective boundary conditions. Stretching the boundary to dampen the unsteady waves is another way to minimize reflections. Grid clustering near the plates does a better job of capturing the unsteady flow field than cases using uniform grids as long as the CFL number is less than one for a sufficient portion of the grid. Results for various stagger angles and oscillation frequencies show good agreement with linear theory as long as the grid is properly resolved.
Document ID
19920006759
Acquisition Source
Legacy CDMS
Document Type
Conference Paper
Authors
Huff, Dennis L.
(NASA Lewis Research Center Cleveland, OH, United States)
Date Acquired
September 6, 2013
Publication Date
January 1, 1992
Subject Category
Aerodynamics
Report/Patent Number
NASA-TM-105406
AIAA PAPER 92-0145
E-6811
NAS 1.15:105406
Report Number: NASA-TM-105406
Report Number: AIAA PAPER 92-0145
Report Number: E-6811
Report Number: NAS 1.15:105406
Meeting Information
Meeting: Aerospace Sciences Meeting and Exhibit
Location: Reno, NV
Country: United States
Start Date: January 6, 1992
End Date: January 9, 1992
Sponsors: AIAA
Accession Number
92N15977
Funding Number(s)
PROJECT: RTOP 535-03-10
Distribution Limits
Public
Copyright
Public Use Permitted.
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