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Title: Surface curvature effects on flow and heat transfer from a round impinging jet

Book ·
OSTI ID:428137
;  [1];  [2]
  1. Inje Univ., Kyungnam (Korea, Republic of). Dept. of Mechanical Engineering
  2. Pusan National Univ. (Korea, Republic of). Research Inst. of Mechanical Technology

Effects of the hemispherically convex surface curvature on the local heat transfer from a round impinging jet were experimentally investigated. The flow at the nozzle exit has a fully developed velocity profile. The jet Reynolds number (Re) ranges from 11,000 to 50,000, the nozzle-to-surface distance (L/d) from 2 to 10, and the hemisphere-to-nozzle diameter ratio (D/d) from 11.2 to 29.3. The results show that the stagnation point Nusselt number (Nu{sub st}) increases with increasing curvature (i.e., decreasing value of D/d). The maximum Nusselt number at the stagnation point occurs at L/d {approx_equal} 6 to 8 for all Re`s and D/d`s tested. Nu{sub st} are well correlated with Re, L/d, and D/d. For larger L/d, Nu{sub st} dependency on Re is stronger due to an increase of turbulence in the approaching jet as a result of the more active exchange of momentum with a surrounding air. The local Nusselt number decreases monotonically from its maximum value at the stagnation point. However, for L/d = 2 and Re = 23,000, and for L/d {le} 4 and Re = 50,000, the streamwise Nusselt number distributions exhibit secondary maxima at r/d {approx_equal} 2.2.

Sponsoring Organization:
Korea Science and Engineering Foundation (Korea, Republic of)
OSTI ID:
428137
Report Number(s):
CONF-960815-; ISBN 0-7918-1506-4; TRN: IM9708%%466
Resource Relation:
Conference: 31. national heat transfer conference, Houston, TX (United States), 3-6 Aug 1996; Other Information: PBD: 1996; Related Information: Is Part Of ASME proceedings of the 31. national heat transfer conference: Volume 2. HTD-Volume 324; Oosthuizen, P.H.; Bayazitoglu, Y.; Ebadian, M.A.; Jones, P.; Avedesian, C.T.; Peterson, J. [eds.]; PB: 210 p.
Country of Publication:
United States
Language:
English

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