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NACA-TM-1050

Heat Transfer Over the Circumference of a Heated Cylinder in Transverse Flow

Organization:
NASA - National Aeronautics and Space Administration (NASA)
Year: 1943

Abstract: A method for recording the local heat-transfer coefficients on bodies in flow was developed. The cylinder surface was kept at constant temperature by the condensation of vapor except for a narrow strip which is heated separately to the same temperature by electricity. The heat-transfer coefficient at each point was determined from the electric heat output and the temperature increase. The distribution of the heat transfer along the circumference of cylinders was recorded over a range of Reynolds numbers of from 5000 to 426,000. The pressure distribution was measured at the same time. At Reynolds numbers up to around 100,000 high maximums of the heat transfer occurred in the forward stagnation point at and on the rear side at 180C, while at around 80 the heat-transfer coefficient on both sides of the cylinder behind the forward stagnation point manifested distinct minimums. Two other maximums occurred at around 115 C behind the forward stagnation point between 170,000 and 426,000. At 426,000 the heat transfer at the location of those maximums was almost twice as great as in the forward stagnation point, and the rear half of the cylinder diffused about 60 percent of the entire heat, The tests are compared with the results of other experimental and theoretical investigations.
URI: https://yse.yabesh.ir/std/handle/yse/29177
Subject: HEAT TRANSFER
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    NACA-TM-1050

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contributor authorNASA - National Aeronautics and Space Administration (NASA)
date accessioned2017-09-04T15:28:09Z
date available2017-09-04T15:28:09Z
date copyright15980
date issued1943
identifier otherNTONEEAAAAAAAAAA.pdf
identifier urihttps://yse.yabesh.ir/std/handle/yse/29177
description abstractA method for recording the local heat-transfer coefficients on bodies in flow was developed. The cylinder surface was kept at constant temperature by the condensation of vapor except for a narrow strip which is heated separately to the same temperature by electricity. The heat-transfer coefficient at each point was determined from the electric heat output and the temperature increase. The distribution of the heat transfer along the circumference of cylinders was recorded over a range of Reynolds numbers of from 5000 to 426,000. The pressure distribution was measured at the same time. At Reynolds numbers up to around 100,000 high maximums of the heat transfer occurred in the forward stagnation point at and on the rear side at 180C, while at around 80 the heat-transfer coefficient on both sides of the cylinder behind the forward stagnation point manifested distinct minimums. Two other maximums occurred at around 115 C behind the forward stagnation point between 170,000 and 426,000. At 426,000 the heat transfer at the location of those maximums was almost twice as great as in the forward stagnation point, and the rear half of the cylinder diffused about 60 percent of the entire heat, The tests are compared with the results of other experimental and theoretical investigations.
languageEnglish
titleNACA-TM-1050num
titleHeat Transfer Over the Circumference of a Heated Cylinder in Transverse Flowen
typestandard
page28
statusActive
treeNASA - National Aeronautics and Space Administration (NASA):;1943
contenttypefulltext
subject keywordsHEAT TRANSFER
subject keywordsHEAT TRANSFER COEFFICIENTS
subject keywordsHEAT TRANSMISSION
subject keywordsHIGH TEMPERATURE TESTS
subject keywordsREYNOLDS NUMBER
subject keywordsTRANSVERSE WAVES
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