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Experimental Heat Transfer
A Journal of Thermal Energy Generation, Transport, Storage, and Conversion
Volume 36, 2023 - Issue 7
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Research Article

Thermal-hydraulic characteristics of a PCHE with zigzag microchannel for hypersonic precooled aero-engines: an experimental study

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Pages 1012-1033 | Received 09 Feb 2022, Accepted 31 May 2022, Published online: 23 Jun 2022
 

ABSTRACT

The PCHE has been recognized as a promising heat exchanger for hypersonic precooled aero-engines due to its superior thermal performance, high compactness and robustness. The present work focuses on the experimental thermal-hydraulic performance study of a novel zigzag microchannel PCHE. The results indicate that the pressure loss caused by friction is the main source. The Fanning correlation proposed by Moisseysev shows more precise prediction results, whose prediction deviations are within 10.0%. The measured Nu is markedly 1.24 ~ 1.94 times higher than that of the straight channel and a new Nu correlation was developed and the maximum deviations do not exceed 5%.

Disclosure statement

The authors declare that they have no known competing financial interests or personal relationships that could have appeared to influence the work reported in this paper.

Nomenclature

wc=

channel width, mm

dc=

channel depth, mm

tp=

plate width, mm

tf=

fin thickness, mm

dh=

hydraulic diameter, mm

tw=

wall thickness, mm

t=

normalized fin thickness

m=

defined dimensionless number

As=

heat transfer area, m2

Ac=

cross area, m2

L=

channel length, m

P=

pressure, Pa

T=

temperature, K

ΔP=

pressure drop, Pa

ΔT=

Temperature difference

U=

overall heat transfer coefficient

K=

form loss coefficient

Q=

heat transfer rate, W

m˙=

mass flow rate, kg/s

G=

mass flow flux, kg/m2s

ρ=

density, kg/m3

k=

thermal conductivity, w/mk

μ=

dynamic viscosity, Ns/m2

lp=

pitch length, mm

np=

number of pitch

ns=

number of sheet

nc=

number of channels per sheet

Cp=

specific heat capacity at constant pressure  J/kgk

D=

diameter of manifold

Re=

Reynolds number

Nu=

Nusselt number

f=

Fanning friction factor

PWR=

power-weight ratio

Pr=

Prandtl number

Greek letters

ε=

effectiveness

nf=

fin efficiency

ηt=

overall fin surface efficiency

α=

heat transfer coefficient, W/m2K

θ=

pitch angle, mm

Subscripts

in=

inlet

out=

outlet

h=

hot side

c=

cold side

W=

metal wall

lm=

log mean temperature difference

max=

maximum

min=

minimum

core=

heat exchanger core

Abbreviations

NTU=

Number of Transfer Units

PCHE=

printed circuit heat exchanger

Additional information

Funding

This paper is supported by the Advanced Jet Propulsion Creativity Center, AEAC, China (HKCX2019-01-004);Young Elite Scientists Sponsorship Program, CAST, China (YESS20210136).

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