A method of computing the transient temperature of thick walls from arbitrary variation of adiabatic-wall temperature and heat-transfer coefficient / by P.R. Hill.

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Bibliographic Details
Main Author:	Hill, Paul R.
Corporate Authors:	Langley Aeronautical Laboratory, United States. National Advisory Committee for Aeronautics
Format:	Government Document Book
Language:	English
Published:	Washington : National Advisory Committee for Aeronautics, [1957]
Series:	Technical note (United States. National Advisory Committee for Aeronautics) ; 4105.
Subjects:	Heat > Transmission > Mathematical models > Methodology. Aerodynamic heating > Mathematical models > Methodology. Airplanes > Materials > Thermal properties > Mathematical models > Methodology. Airplanes > Materials > Surfaces > Mathematical models > Methodology.

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Call Number:	Y 3.N 21/5:6/4105
Y 3.N 21/5:6/4105	Available Place a Hold