The work presents results of numerical investigation of flow structure and heat transfer of unconfined and confined impact mist jets with low mass fraction of droplets (ML1≤1%). The downward gas-droplets jet is issued from a pipe and strikes into the center of the circular target wall. Mathematical model is based on the solution to RANS equations for the two-phase flow in Euler approximation. For the calculation of the fluctuation characteristics of the dispersed phase model equations of Derevich and Zaichik [1] and Zaichik et al. [2] were applied. Predictions were performed for the distances between the nozzle and the target plate x/(2R) = 0.5–10 and the initial droplets size (d1 = 5–100 μm) at the fixed Reynolds number based on the nozzle diameter, Re = 26600. Addition of droplets causes significant increase of heat transfer intensity in the vicinity of the jet stagnation point compared with the one-phase air impact jet.
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2010 14th International Heat Transfer Conference
August 8–13, 2010
Washington, DC, USA
Conference Sponsors:
- Heat Transfer Division
ISBN:
978-0-7918-4940-8
PROCEEDINGS PAPER
Numerical Study of Flow and Heat Transfer in Confined and Unconfined Round Mist Impinging Jet
Viktor I. Terekhov,
Viktor I. Terekhov
Kutateladze Institute of Thermophysics SB RAS, Novosibirsk, Russia
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Maksim A. Pakhomov
Maksim A. Pakhomov
Kutateladze Institute of Thermophysics SB RAS, Novosibirsk, Russia
Search for other works by this author on:
Viktor I. Terekhov
Kutateladze Institute of Thermophysics SB RAS, Novosibirsk, Russia
Maksim A. Pakhomov
Kutateladze Institute of Thermophysics SB RAS, Novosibirsk, Russia
Paper No:
IHTC14-22162, pp. 491-499; 9 pages
Published Online:
March 1, 2011
Citation
Terekhov, VI, & Pakhomov, MA. "Numerical Study of Flow and Heat Transfer in Confined and Unconfined Round Mist Impinging Jet." Proceedings of the 2010 14th International Heat Transfer Conference. 2010 14th International Heat Transfer Conference, Volume 5. Washington, DC, USA. August 8–13, 2010. pp. 491-499. ASME. https://doi.org/10.1115/IHTC14-22162
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