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Experimental Heat Transfer
A Journal of Thermal Energy Generation, Transport, Storage, and Conversion
Volume 35, 2022 - Issue 3
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Research Article

Investigations on the effect of disturbed flow using differently configured turbulators and Alumina nanofluid as a coolant in a double tube heat exchanger

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Pages 282-307 | Received 13 Jul 2020, Accepted 01 Dec 2020, Published online: 03 Jan 2021
 

ABSTRACT

This paper investigates the effect of the combined passive technique on heat transfer enhancement, friction factor, and thermal performance of a double-tube heat exchanger fitted with differently configured turbulators and using Alumina nanofluid. The performance parameters are studied for fixed flow rate (Re = 2500) of water at constant heat flux in the inner tube (hot fluid) and varying flow rates (500≤ Re≤5000) of Alumina nanofluid (volume concentrations: 0.05–0.15%) flowing in the outer tube (cold fluid). The configurations tested are a peripherally V-cut twisted tape (Twist Ratio = 20, 13.3, and 9.8) and a propeller turbulator (Number of propellers: 6, 8, and 10). The results show increased Nusselt number by 22.4% and 29.43%, increased Thermal Performance Factor by 1.25 and 1.33, respectively, for decreased twist ratio and increased number of propellers and volume concentration of Alumina nanofluid. The peripherally V-cut twisted tape (TR = 9.8) and propeller turbulator (Number of propellers = 10) with 0.15% volume concentrations of Alumina nanofluid combination give better performance, with a slight penalty in pressure drop. The correlations for the Nusselt number and friction factor are developed from the experimental data, which are fairly in good agreement with the experimental data.

Graphical abstract

Acknowledgments

This work is supported by the Vision Group on Science and Technology (VGST), State Government of Karnataka, India, for the funding granted under the KFIST-L1 scheme (GRD No: 476).

Nomenclature

Cp=

Specific heat, J kg−1K−1

d=

Diameter, m.

D=

Tape width, m

f=

friction factor

h=

heat transfer coefficient, W m−2 k−1

H=

Pitch length of tape, m

K=

Thermal conductivity, W m−1k−1

L=

Length, m.

n=

Sample size

Nu=

Nusselt number

Pr=

Prandtl number

Q=

Heat transfer

Re=

Reynolds Number

T=

Temperature, O.C.

U=

Uncertainty

V=

Velocity, m s−1

X=

Sample mean

ΔP=

Pressure Drop, psi or bar

Greek/Roman/Latin Letters=
Ρ=

Density, kg m−3

μ=

Dynamic viscosity, kg-m s−1

ϕ=

Volume concentration

σ=

Standard deviation

Subscripts=
i=

inlet

o=

outlet

c=

cold fluid

h=

hot fluid

f=

fluid

m=

mass

nf=

nanofluid

P=

Particle

W=

Water

fhot=

hot side friction factor

fcold=

cold side friction factor

NP=

Number of propellers

Abbreviations=
DTHE=

Double Tube Heat Exchanger

ID=

Inner Diameter

LMTD=

Logarithmic Mean Temperature Difference

OD=

Outer Diameter

TPF=

Thermal Performance Factor

TR=

Twist Ratio

Additional information

Funding

This work was supported by the Vision Group on Science and Technology (VGST), Karnataka, India [KFIST-L1 scheme bearing GRD No 476].

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