Bénard, Emmanuel and Cooper, Richard K. and Sidorenko, A. Transitional and turbulent heat transfer of swept cylinder attachment line in hypersonic flow. (2006) International Journal of Heat and Mass Transfer, vol. 49 (n° 5-6). pp. 836-843. ISSN 0017-9310
(Document in English)
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A wide range of experimental results carried out in low enthalpy facilities is used to sustain simple correlations predicting heat transfer rates on an attachment line in hypersonic flow. It is observed that for long swept cylinders a nearly asymptotic state can be reached for which transition Reynolds number does not change substantially quite far from the apex of the cylinder. Intermittency based on measured heat fluxes was used to describe the laminar-turbulent process. Prediction of turbulent heat transfer rates is established using a reference temperature method that provides quick and relatively accurate estimates for a wide range of Mach number and temperature ratio.
|Additional Information:||Thanks to Elsevier editor. The definitive version is available at http://www.sciencedirect.com The original PDF of the article can be found at International Journal of Heat and Mass Transfer website: http://www.sciencedirect.com/science/journal/00179310|
|Audience (journal):||International peer-reviewed journal|
|Institution:||Université de Toulouse > Institut Supérieur de l'Aéronautique et de l'Espace - ISAE (FRANCE)|
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|Deposited By:||Emmanuel Benard|
|Deposited On:||08 Mar 2011 10:58|
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