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SL4 code - A user's manualThe SL-4 code is a computer automated scheme for solving the equations describing the fully-coupled viscous, radiating flow over the front face of a blunt body which may or may not be ablating. The code provides a basis for obtaining predictions of the surface beating to a body entering any planetary atmosphere at hyperbolic velocities. The code is written in FORTRAN V and is operational on both the Univac 1108 (EXEC 8) system in use at LMSC and the CDC 7600 system in use at the University of California, Berkeley. An overview of the SL-4 code computational logic flow, a description of the input requirements and output results, and comments on the practical use of the code are presented. As such this report forms a users manual for operation of the SL-4 code.
Document ID
19730012209
Acquisition Source
Legacy CDMS
Document Type
Contractor Report (CR)
Authors
Chou, Y. S.
(Lockheed Missiles and Space Co. Sunnyvale, CA, United States)
Date Acquired
September 2, 2013
Publication Date
March 1, 1973
Publication Information
Publisher: NASA
Subject Category
Thermodynamics And Combustion
Report/Patent Number
NASA-CR-2235
Report Number: NASA-CR-2235
Accession Number
73N20936
Funding Number(s)
CONTRACT_GRANT: NAS2-6668
Distribution Limits
Public
Copyright
Work of the US Gov. Public Use Permitted.
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