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Heat transfer suppression during impact jet interaction with hemispherical cavity

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Abstract

Heat transfer during impingement of an impact jet onto an obstacle with a hemispherical cavity has been experimentally studied. It is established that the local heat transfer exhibits a significant (two- to threefold) decrease as compared to that on a flat surface. A probable mechanism of suppression of the turbulent convection is considered and possible methods of heat transfer control are discussed.

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Correspondence to V. I. Terekhov.

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Original Russian Text © V.I. Terekhov, S.V. Kalinina, 2011, published in Pis’ma v Zhurnal Tekhnicheskoi Fiziki, 2011, Vol. 37, No. 20, pp. 87–94.

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Terekhov, V.I., Kalinina, S.V. Heat transfer suppression during impact jet interaction with hemispherical cavity. Tech. Phys. Lett. 37, 984–987 (2011). https://doi.org/10.1134/S1063785011100270

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  • DOI: https://doi.org/10.1134/S1063785011100270

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