The differential equation describing the temperature pro file in the carbon zone of a charring ablator was simulated on an IBM 7040 digital computer using MIMIC, a digital- analog simulator language. This differential equation de scribes a nonlinear, two-point boundary value problem, thus requiring an iterative procedure to converge to a solu tion. In order to handle the iterative procedure, the logical- control-variable feature of MIMIC was especially useful.
Get full access to this article
View all access options for this article.
References
1.
G.C. AprilEgdelvalle R.W. PikeSolution of the frozen flow energy equation Reacting Fluids Laboratory status report NASA-RFL-2Louisiana State University July 1 1966
2.
K.M. KratschL.F. HearneH.R. McChesneyThermal performance of heat shield composites during planetaryentry Lockheed Missiles & Space CompanySunnyvale California October 1963
3.
4.
R.G. WilsonThermophysical properties of six charring ablators from 140° to 700°K and two chars from 800° to 3000° K TND-2991NASA October 1965
5.
H.E. PetersenF.J. SansomMIMIC a digital simulator program Sesca internal memo 65-12 May 1965
6.
R.W. PikeEvaluation of the literature for chemical reactions and the reaction rates for the decomposition products from charring ablators LWP 181NASA January 21 1966
7.
G.C. AprilEgdelvalle R.W. PikeSolution of the frozen flow momentum equation Reacting Fluids Laboratory status report NASA-RFL-5Louisiana State University October 1 1966