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Unsteady three-dimensional thermal field prediction in turbine blades using nonlinear BEMA time-and-space accurate and computationally efficient fully three dimensional unsteady temperature field analysis computer code has been developed for truly arbitrary configurations. It uses boundary element method (BEM) formulation based on an unsteady Green's function approach, multi-point Gaussian quadrature spatial integration on each panel, and a highly clustered time-step integration. The code accepts either temperatures or heat fluxes as boundary conditions that can vary in time on a point-by-point basis. Comparisons of the BEM numerical results and known analytical unsteady results for simple shapes demonstrate very high accuracy and reliability of the algorithm. An example of computed three dimensional temperature and heat flux fields in a realistically shaped internally cooled turbine blade is also discussed.
Document ID
19940019192
Acquisition Source
Legacy CDMS
Document Type
Conference Paper
Authors
Martin, Thomas J.
(Pennsylvania State Univ. University Park, PA, United States)
Dulikravich, George S.
(Pennsylvania State Univ. University Park, PA, United States)
Date Acquired
September 6, 2013
Publication Date
November 1, 1993
Publication Information
Publication: NASA. Lewis Research Center, The Fifth Annual Thermal and Fluids Analysis Workshop
Subject Category
Fluid Mechanics And Heat Transfer
Accession Number
94N23665
Distribution Limits
Public
Copyright
Work of the US Gov. Public Use Permitted.
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