1970
DOI: 10.1016/0017-9310(70)90153-5
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Heat transfer through the axially symmetric boundary layer on a moving circular fibre

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Cited by 59 publications
(17 citation statements)
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“…The results obtained from our analysis are in good agreement with those of Crane [4], as shown in Fig 2. The accuracy of the Pohlhausen method increases with increasing values of x, that is increased axial distance from the orifice. It is also important to note that for a Prandtl number equal to unity the results match up with those of Bourne and Elliston [3]. This paper has shown that the Pohlhausen method can be a powerful tool in predicting the rate of heat transfer from the surface of a cylindrical fibre moving through a stationary fluid at large distances from the orifice.…”
Section: Resultssupporting
confidence: 71%
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“…The results obtained from our analysis are in good agreement with those of Crane [4], as shown in Fig 2. The accuracy of the Pohlhausen method increases with increasing values of x, that is increased axial distance from the orifice. It is also important to note that for a Prandtl number equal to unity the results match up with those of Bourne and Elliston [3]. This paper has shown that the Pohlhausen method can be a powerful tool in predicting the rate of heat transfer from the surface of a cylindrical fibre moving through a stationary fluid at large distances from the orifice.…”
Section: Resultssupporting
confidence: 71%
“…Bourne and Elliston [3] have used a Pohlhausen technique to determine the rate of heat transfer from a moving cylindrical fibre for Prandtl numbers in the range 0 ≤ σ ≤ 1. This paper aims to build upon the work of Bourne and Elliston [3] by determining the Nusselt number for a range of Prandtl numbers greater than unity. The method used is similar to that of Bourne and Elliston, with the same assumptions made with respect to fibre velocity, temperature and radius.…”
Section: Initial Observationsmentioning
confidence: 99%
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“…Bourne and Elliston [8] studies heat transfer through the axially symmetric boundary layer on a moving circular fibre. Krani and Pecho [27] reported on the thermal laminar boundary layer on a continuous cylinder.…”
Section: Introductionmentioning
confidence: 99%
“…' dt dz dr) Pa dz ar r dr a Z ) energy ( dT dTa'\ id( dTa d( dTa\ CpaPa Va + Ua = _Trka ) + ka ) (12) where cpa is the specific heat for the air, ka is the thermal conductivity for the fluid, ua and Va are the radial and axialvelocities of the air respectively, Ta is the temperature of the air, Va is the kinematic viscosity of the air, and Pa is the air density.…”
Section: Governing Equationsmentioning
confidence: 99%