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Development and application of the GIM code for the Cyber 203 computerThe GIM computer code for fluid dynamics research was developed. Enhancement of the computer code, implicit algorithm development, turbulence model implementation, chemistry model development, interactive input module coding and wing/body flowfield computation are described. The GIM quasi-parabolic code development was completed, and the code used to compute a number of example cases. Turbulence models, algebraic and differential equations, were added to the basic viscous code. An equilibrium reacting chemistry model and implicit finite difference scheme were also added. Development was completed on the interactive module for generating the input data for GIM. Solutions for inviscid hypersonic flow over a wing/body configuration are also presented.
Document ID
19830008405
Acquisition Source
Legacy CDMS
Document Type
Contractor Report (CR)
Authors
Stainaker, J. F.
(Lockheed Missiles and Space Co. Huntsville, AL, United States)
Robinson, M. A.
(Lockheed Missiles and Space Co. Huntsville, AL, United States)
Rawlinson, E. G.
(Lockheed Missiles and Space Co. Huntsville, AL, United States)
Anderson, P. G.
(Lockheed Missiles and Space Co. Huntsville, AL, United States)
Mayne, A. W.
(Lockheed Missiles and Space Co. Huntsville, AL, United States)
Spradley, L. W.
(Lockheed Missiles and Space Co. Huntsville, AL, United States)
Date Acquired
September 4, 2013
Publication Date
December 1, 1982
Publication Information
Publisher: NASA
Subject Category
Fluid Mechanics And Heat Transfer
Report/Patent Number
NASA-CR-3652
NAS 1.26:3652
LMSC-HREC-TD-D784478
Report Number: NASA-CR-3652
Report Number: NAS 1.26:3652
Report Number: LMSC-HREC-TD-D784478
Accession Number
83N16676
Funding Number(s)
CONTRACT_GRANT: NAS1-15783
CONTRACT_GRANT: NAS1-15795
Distribution Limits
Public
Copyright
Work of the US Gov. Public Use Permitted.
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