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Finite element Euler calculations of unsteady transonic cascade flowsA Galerkin finite element procedure incorporating an explicit Runge-Kutta time-stepping scheme has been developed in this work to solve unsteady transonic flow in cascades. The computational domain is discretized by a globally unstructured but locally structured blade-fitted deformable mesh. The Galerkin approximation is applied to the unsteady Euler equations based on a mixed Eulerian-Lagrangian description. The semi-discretized equations are integrated forward in time using a multistage Runge-Kutta scheme. An artificial dissipation operator of the type proposed by Jameson is adapted in the current scheme to capture shocks and suppress nonphysical oscillations. Phase-shifted boundary conditions are used to reduce the computational domain to a single reference passage. Results for both steady and unsteady transonic flows through cascades are presented and compared to existing finite volume solutions.
Document ID
19920053065
Acquisition Source
Legacy CDMS
Document Type
Conference Paper
Authors
Hsiao, Chingteng
(NASA Lewis Research Center Cleveland, OH, United States)
Bendiksen, Oddvar O.
(California, University Los Angeles, United States)
Date Acquired
August 15, 2013
Publication Date
January 1, 1992
Subject Category
Aerodynamics
Report/Patent Number
AIAA PAPER 92-2120
Report Number: AIAA PAPER 92-2120
Meeting Information
Meeting: AIAA Dynamics Specialists Conference
Location: Dallas, TX
Country: United States
Start Date: April 16, 1992
End Date: April 17, 1992
Accession Number
92A35689
Funding Number(s)
CONTRACT_GRANT: NAS3-25574
Distribution Limits
Public
Copyright
Other

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