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Radiant-interchange configuration factors

contributor authorNASA - National Aeronautics and Space Administration (NASA)
date accessioned2017-09-04T18:09:43Z
date available2017-09-04T18:09:43Z
date copyright01/01/1952
date issued1952
identifier otherGVONEEAAAAAAAAAA.pdf
identifier urihttp://yse.yabesh.ir/std;jsery=autho16/handle/yse/192812
description abstractA study is presented of the geometric configuration factors required for computing radiant heat transfer between opaque surfaces separated by a nonabsorbing medium and various methods of determining the configuration factors are discussed. Configuration-factor solutions available in the literature have been checked and the more complicated equations are presented as families of curves. Cases for point, line, and finite-area sources are worked out over a wide range of geometric proportions. These cases include several new configurations involving rectangles, triangles, and cylinders of finite length which are integrated and tabulated. An analysis is presented, in which configuration factors are employed of the radiant heat transfer to the rotor blades of a typical gas turbine under different conditions of temperature and pressure. (author)
languageEnglish
titleNACA-TN-2836num
titleRadiant-interchange configuration factorsen
typestandard
page111
statusActive
treeNASA - National Aeronautics and Space Administration (NASA):;1952
contenttypefulltext
subject keywordsABSORPTION
subject keywordsAIRCRAFT ENGINES
subject keywordsANALYSIS (MATHEMATICS)
subject keywordsCONFIGURATIONS
subject keywordsCOOLING
subject keywordsCYLINDERS
subject keywordsEMISSIVITY
subject keywordsGAS TURBINE ENGINES
subject keywordsGASES
subject keywordsRADIATIVE HEAT TRANSFER
subject keywordsRECTANGLES
subject keywordsROTOR BLADES (TURBOMACHINERY)
subject keywordsSURFACE GEOMETRY
subject keywordsTRIANGLES


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