Regional heat transfer in two-pass and three-pass passages with 180-deg sharp turns
- Carnegie Mellon Univ., Pittsburgh, PA (USA)
The heat transfer distributions for flow passing through two-pass (one-turn) and three-pass (two-turn) passages with 180-deg sharp turns are studied by using the analogous naphthalene mass transfer technique. Both passages have square cross section and length-to-height ratio of 8. The passage surface, including top wall, side walls, and partition walls, is divided into 26 segments for the two-pass passage and 40 segments for the three-pass passage. Mass transfer results are presented for each segment along with regional and overall averages. The very nonuniform mass transfer coefficients measured around a sharp 180-deg turn exhibit the effects of flow separation, reattachment, and impingement, in addition to secondary flows. Results for the three-pass passage indicate that heat transfer characteristics around the second turn are virtually the same as those around the first turn. This may imply that, in a multiple-pass passage, heat transfer at the first turn has already reached the thermally developed (periodic) condition. Over the entire two-pass passage, the heat transfer enhancement induced by the single-turn is about 45 to 65% of the fully developed values in a straight channel. Such as heat transfer enhancement decreases with an increase in Reynolds number. In addition, overall heat transfer of three-pass passage is approximately 15% higher than that of the two-pass one. This 15% increase appears to be Reynolds number independent. The pressure loss induced by the sharp turns is found to be very significant. Within the present testing range, the pressure loss coefficient for both passages is Reynolds number dependent.
- OSTI ID:
- 5645764
- Journal Information:
- Journal of Heat Transfer (Transcations of the ASME (American Society of Mechanical Engineers), Series C); (United States), Vol. 113:1; ISSN 0022-1481
- Country of Publication:
- United States
- Language:
- English
Similar Records
Predictions of flow and heat transfer in sharp 180-deg turns of gas turbine coolant channels with and without turning vanes
Effects of rib arrangements on pressure drop and heat transfer in a rib-roughened channel with a sharp 180 deg turn
Related Subjects
42 ENGINEERING
TURBINE BLADES
COOLING
DATA
FORCED CONVECTION
GAS TURBINE ENGINES
MASS TRANSFER
NAPHTHALENE
AROMATICS
CONDENSED AROMATICS
CONVECTION
ENERGY TRANSFER
ENGINES
HEAT ENGINES
HEAT TRANSFER
HYDROCARBONS
INFORMATION
INTERNAL COMBUSTION ENGINES
ORGANIC COMPOUNDS
330103* - Internal Combustion Engines- Turbine
420400 - Engineering- Heat Transfer & Fluid Flow