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ホーム アーカイブ Thermal Letter 役員 今後の会合 国際伝熱会議の集会

ISBN : 0-89116-130-9

International Heat Transfer Conference 6
1978, 7-11 August, Toronto, Canada

CONVECTION HEAT TRANSFER IN ROTATING CURVED PIPES

Get access DOI: 10.1615/IHTC6.2830
pages 141-146

要約

Heat transfer and fluid flow parameters are combined with ballistic characteristics to construct an analytical model which predicts transient pressures and temperatures of a spacecraft spin system during operation. The components of these systems are mounted on the periphery of a conical structure and hence operate under centripetal and lateral loads which amplify the convection heat transfer. The validity of the analysis is demonstrated by comparing predictions with data obtained during static and dynamic testing of an engineering model for Space Test Program Flight P78-1 spin system.
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