ISSN: (Online) 2321 -4155
ISSN: (Print) 2320 -7000

JOURNAL OF INDIAN RESEARCH
VOLUME : 1, ISSUE : 3 July-September, 2013 (ISSN No. : 2321-4155)
 

A NUMERICAL METHOD TO STUDY THE HEAT TRANSFER IN ROCKET NOZZLE

THROAT BY INVERSE HEAT CONDUCTION TECHNIQUE

A.V.N. Krishna & S. Krishna Murty
 
ABSTRACT
This paper is study of one dimensional heat conduction with thermo- physical properties K, ROW, Cp of a material varying with temperature. The physical problem is characterized by a slab of infinite length and thickness L, imposed with a net heat flux at x=0, with the other end being insulated. The problem is solved by using Inverse Heat Conduction Technique (IHCP).
 
KEYWORD
Duhamel’s theorem, Heat Conduction, Sensitivity Coefficient, Taylor series, tridiogonal system.
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