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User's guide for the computer code COLTS for calculating the coupled laminar and turbulent flow over a Jovian entry probeA user's guide for a computer code 'COLTS' (Coupled Laminar and Turbulent Solutions) is provided which calculates the laminar and turbulent hypersonic flows with radiation and coupled ablation injection past a Jovian entry probe. Time-dependent viscous-shock-layer equations are used to describe the flow field. These equations are solved by an explicit, two-step, time-asymptotic finite-difference method. Eddy viscosity in the turbulent flow is approximated by a two-layer model. In all, 19 chemical species are used to describe the injection of carbon-phenolic ablator in the hydrogen-helium gas mixture. The equilibrium composition of the mixture is determined by a free-energy minimization technique. A detailed frequency dependence of the absorption coefficient for various species is considered to obtain the radiative flux. The code is written for a CDC-CYBER-203 computer and is capable of providing solutions for ablated probe shapes also.
Document ID
19820024762
Acquisition Source
Legacy CDMS
Document Type
Technical Memorandum (TM)
Authors
Kumar, A.
(Old Dominion Univ. Hampton, VA, United States)
Graeves, R. A.
(NASA Langley Research Center)
Date Acquired
September 4, 2013
Publication Date
June 1, 1980
Subject Category
Fluid Mechanics And Heat Transfer
Report/Patent Number
NASA-TM-81848
NAS 1.15:81848
Report Number: NASA-TM-81848
Report Number: NAS 1.15:81848
Accession Number
82N32638
Funding Number(s)
PROJECT: RTOP 506-51-23-01
Distribution Limits
Public
Copyright
Work of the US Gov. Public Use Permitted.
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