Accession Number : AD0461662


Title :   SOLUTION OF TRANSIENT HEAT TRANSFER PROBLEMS FOR FLAT PLATES, CYLINDERS, AND SPHERES BY FINITE-DIFFERENCE METHODS


Descriptive Note : Progress rept.,


Corporate Author : ARMY MISSILE COMMAND REDSTONE ARSENAL AL SYSTEMS RESEARCH DIRECTORATE


Personal Author(s) : Burleson, W G ; Eppes, Jr, R


Full Text : https://apps.dtic.mil/dtic/tr/fulltext/u2/461662.pdf


Report Date : 15 Mar 1965


Pagination or Media Count : 42


Abstract : This report presents finite-difference (forward) heat transfer equations applicable to transient, radial heat flow in spheres and cylinders and applicable to transient, one-dimensional heat flow in flat plates. By minor manipulations, a single heat transfer procedure can be utilized easily to determine the transient heat flow in all three basic structure configurations. For each skin configuration the accuracy of the finite-difference procedure, compared with exact analytical methods, depends on optimum selection of the calculation time increment and the incremental distance between temperature nodes in relation to the material thermal properties and on the closeness of the approximate temperature gradients to the true gradients.


Descriptors :   *CURVED PROFILES , *HEAT TRANSFER , AERODYNAMIC CONFIGURATIONS , AERODYNAMIC HEATING , AIRFRAMES , CYLINDRICAL BODIES , EQUATIONS , FLAT PLATE MODELS , GUIDED MISSILES , MATHEMATICAL ANALYSIS , NOSE CONES , NUMERICAL METHODS AND PROCEDURES , ONE DIMENSIONAL FLOW , REENTRY VEHICLES , SELECTION , SPHERES , SURFACE TEMPERATURE , THERMAL PROPERTIES , THERMAL STRESSES


Subject Categories : Theoretical Mathematics
      Thermodynamics


Distribution Statement : APPROVED FOR PUBLIC RELEASE