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An implicit finite-difference code for inviscid and viscous cascade flowAn implicit finite-difference code is developed to solve either inviscid or viscous flow about two-dimensional cascade blade elements. General coordinate transformations are used so that boundaries can coincide with coordinate lines, and an automatic grid generation routine based on elliptic partial differential equations is employed to mesh arbitrary cascade elements. Characteristic combinations of the differential equations are used at inflow and outflow boundaries. Computed results for both inviscid and viscous flow are compared with other existing cascade solutions and experimental data.
Document ID
19800059958
Acquisition Source
Legacy CDMS
Document Type
Conference Paper
Authors
Steger, J. L.
(Flow Simulations, Inc. Sunnyvale, Calif., United States)
Pulliam, T. H.
(NASA Ames Research Center Moffett Field, Calif., United States)
Chima, R. V.
(NASA Lewis Research Center Cleveland, Ohio, United States)
Date Acquired
August 10, 2013
Publication Date
July 1, 1980
Subject Category
Aerodynamics
Report/Patent Number
AIAA PAPER 80-1427
Report Number: AIAA PAPER 80-1427
Meeting Information
Meeting: Fluid and Plasma Dynamics Conference
Location: Snowmass, CO
Start Date: July 14, 1980
End Date: July 16, 1980
Sponsors: American Institute of Aeronautics and Astronautics
Accession Number
80A44128
Distribution Limits
Public
Copyright
Other

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