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ISSN Online: 2377-424X

International Heat Transfer Conference 3
August, 7-12, 1966, Chicago, USA

HEAT TRANSFER FROM OXYGEN AT HIGH TEMPERATURES

Get access (open in a dialog) DOI: 10.1615/IHTC3.570
pages 306-315

Sinopsis

A theoretical and experimental investigation is reported of the heat transfer to the end wall of a shock tube behind a reflected shock wave in oxygen under conditions ranging from zero to nearly complete dissociation. Predictions of the temperature rise at the end wall as a function of the shock heated gas temperature are shown to be in good agreement with experimental measurements using thin film heat gauges over a temperature range of 500−4300°K. Results are also presented for air up to 2000°K. Failure to account for convection in the analysis is shown to lead to a significant overestimation of its thermal conductivity.