Heat and Mass Transfer

, Volume 49, Issue 5, pp 679–694

On flow structure, heat transfer and pressure drop in varying aspect ratio two-pass rectangular channel with ribs at 45°

  • Waseem Siddique
  • Igor V. Shevchuk
  • Lamyaa El-Gabry
  • Narmin B. Hushmandi
  • Torsten H. Fransson
Original

DOI: 10.1007/s00231-013-1111-5

Cite this article as:
Siddique, W., Shevchuk, I.V., El-Gabry, L. et al. Heat Mass Transfer (2013) 49: 679. doi:10.1007/s00231-013-1111-5

Abstract

To increase the thermal efficiency of gas turbines, inlet temperature of gas is increased. This results in the requirement of cooling of gas turbine blades and vanes. Internal cooling of gas turbine blades and vanes is one of several options. Two-pass channels are provided with ribs to enhance heat transfer at the expense of an increased pressure drop. The space in the blade is limited and requires channels with small aspect ratios. Numerical simulations have been performed to investigate heat transfer, flow field and pressure loss in a two-pass channel equipped with 45° ribs with aspect ratio (Win/H) equal to 1:3 in the inlet pass and 1:1 in the outlet pass with both connected together with a 180° bend. The results are compared with a higher aspect ratio channel (Win/H = 1:2, inlet pass). In the ribbed channel, a decrease in pressure drop was observed with a decrease in the aspect ratio of the channel. The smaller aspect ratio channel not only allows using more cooling channels in the blade, but also results in more heat transfer enhancement. The divider-to-tip wall distance (Wel) has influence on the pressure drop, as well as on the heat transfer enhancement at the bend and outlet pass. Heat transfer decreases with decrease in aspect ratio of the inlet pass of the two-pass channel. With increase in divider-to-tip wall distance, heat transfer tries to attain a constant value.

Abbreviations

Cp

Isobaric specific heat (J/kg K)

D

Diameter (m)

e

Rib height (m)

f

Friction factor

h

Heat transfer coefficient [W/(m2K)]

H

Height of the channel (m)

k

Thermal conductivity of the fluid [W/(m K)]

Nu

Nusselt number (h Dh/k)

P

Pitch between ribs (m)

p

Pressure (Pa)

Pr

Prandtl Number (Cpμ/k)

Re

Reynolds number (ρUinDh/μ)

T

Temperature (K)

U

Velocity magnitude (m/s)

W

Width (m)

Greek symbols

Δ

Difference

μ

Dynamic viscosity (kg/s m)

ρ

Density (kg/m3)

Subscripts

avg.

Average

el

Divider-to-tip wall

in

Inlet

out

Outlet

0

Dittus-Boelter correlation

st

Averaged Nusselt Number of a straight channel

web

Divider wall

Copyright information

© Springer-Verlag Berlin Heidelberg 2013

Authors and Affiliations

  • Waseem Siddique
    • 1
    • 2
  • Igor V. Shevchuk
    • 3
  • Lamyaa El-Gabry
    • 4
  • Narmin B. Hushmandi
    • 1
  • Torsten H. Fransson
    • 1
  1. 1.Department of Energy TechnologyRoyal Institute of Technology (KTH)StockholmSweden
  2. 2.Department of Nuclear EngineeringPakistan Institute of Engineering and Applied Sciences (PIEAS)IslamabadPakistan
  3. 3.MBtech Group GmbH & Co. KGaAFellbach-SchmidenGermany
  4. 4.Department of Mechanical EngineeringAmerican University in Cairo (AUC)CairoEgypt

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