Publication Cover
Experimental Heat Transfer
A Journal of Thermal Energy Generation, Transport, Storage, and Conversion
Volume 35, 2022 - Issue 7
486
Views
7
CrossRef citations to date
0
Altmetric
Research Article

Heat transfer characteristics of flat and concave surfaces by circular and elliptical jet impingement

&
Pages 938-963 | Received 28 May 2021, Accepted 14 Oct 2021, Published online: 01 Nov 2021
 

ABSTRACT

The present paper reports the thermal behavior of flat and curved surfaces with impinging jets employing circular and elliptical nozzle for identical equivalent diameter (de). Tests are performed with the Reynolds number varying from 11,250–22,500, varied range of plate to nozzle distance (z/d = 1–6), various nozzle aspect ratios (AR = 1–4). A comparison of thermal behavior between flat and concave surfaces (d/D = 0.05) is discussed in this study. The maximum enhancement in the stagnation Nusselt number found to be 27.4% and 24.8% with the increase in AR = 1 to 4 for flat surface, curved surface, respectively.

Disclosure statement

No potential conflict of interest was reported by the author(s).

Nomenclature

a=

Major axis length of nozzle, mm

As=

Surface area of test foil, m2

b=

Minor axis length of nozzle, mm

de=

Equivalent diameter of the nozzle, mm

D=

Test surface diameter, mm

I=

Current passing through test foil, A

k=

Thermal conductivity of cooling fluid (air), W m−1 K−1

m=

Mass flow rate of air, kg s−1

Nu=

Nusselt number

P=

The pressure in airline, kg m−1 s−2

Q=

Flow rate of air, m3 s−1

q”conv=

Heat flux taken by the impinging jet, W m−2

q”gen=

Heat generated by the joule heating, W m−2

q”loss=

Heat loss from the surface, W m−2

s=

Distance in the circumferential direction, mm

t=

Thickness of test surface, mm

Tamb=

Ambient temperature, K

Taw=

Adiabatic wall temperature, K

V=

Voltage drops across the test foil, V

x=

Distance in the longitudinal direction, mm

z=

Nozzle to plate distance, mm

z/d=

Non-dimensionless nozzle to plate distance

Greek Symbols=
ε=

Emissivity of a test surface

μ=

Dynamic viscosity of cooling fluid (air), Kg m−1 s−1

ρ=

Density of cooling fluid (air), kg m3

Subscripts=
gen=

Heat generation

loss=

Heat loss

stag=

Stagnation

sur=

Surface

Additional information

Funding

The author(s) reported there is no funding associated with the work featured in this article.

Log in via your institution

Log in to Taylor & Francis Online

PDF download + Online access

  • 48 hours access to article PDF & online version
  • Article PDF can be downloaded
  • Article PDF can be printed
USD 61.00 Add to cart

Issue Purchase

  • 30 days online access to complete issue
  • Article PDFs can be downloaded
  • Article PDFs can be printed
USD 352.00 Add to cart

* Local tax will be added as applicable

Related Research

People also read lists articles that other readers of this article have read.

Recommended articles lists articles that we recommend and is powered by our AI driven recommendation engine.

Cited by lists all citing articles based on Crossref citations.
Articles with the Crossref icon will open in a new tab.