An Approximate Solution to the Shuttle Heat-Transfer Losses in a Reciprocating MachineSource: Journal of Engineering for Gas Turbines and Power:;1971:;volume( 093 ):;issue: 002::page 177Author:P. A. Rios
DOI: 10.1115/1.3445549Publisher: The American Society of Mechanical Engineers (ASME)
Abstract: The axial heat transfer due to the oscillatory motion of a long displacer in a cylinder with an axial temperature gradient is treated. The effect of the resistance to heat transfer due to the radial clearance between the displacer and the cylinder is considered, as well as the effect of a limited thermal diffusivity in the walls. A method for the estimation of the effect of the gas flow in the clearance volume is presented. A simple approximate solution is obtained by linearization and application of Fourier series. The effect of radial clearance, material properties, length, and wall thickness on the net heat transfer rate is discussed.
keyword(s): Heat transfer , Machinery , Clearances (Engineering) , Cylinders , Fourier series , Wall thickness , Temperature gradients , Motion , Electrical resistance , Gas flow , Thermal diffusivity AND Materials properties ,
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contributor author | P. A. Rios | |
date accessioned | 2017-05-09T00:56:50Z | |
date available | 2017-05-09T00:56:50Z | |
date copyright | April, 1971 | |
date issued | 1971 | |
identifier issn | 1528-8919 | |
identifier other | JETPEZ-26692#177_1.pdf | |
identifier uri | http://yetl.yabesh.ir/yetl/handle/yetl/151111 | |
description abstract | The axial heat transfer due to the oscillatory motion of a long displacer in a cylinder with an axial temperature gradient is treated. The effect of the resistance to heat transfer due to the radial clearance between the displacer and the cylinder is considered, as well as the effect of a limited thermal diffusivity in the walls. A method for the estimation of the effect of the gas flow in the clearance volume is presented. A simple approximate solution is obtained by linearization and application of Fourier series. The effect of radial clearance, material properties, length, and wall thickness on the net heat transfer rate is discussed. | |
publisher | The American Society of Mechanical Engineers (ASME) | |
title | An Approximate Solution to the Shuttle Heat-Transfer Losses in a Reciprocating Machine | |
type | Journal Paper | |
journal volume | 93 | |
journal issue | 2 | |
journal title | Journal of Engineering for Gas Turbines and Power | |
identifier doi | 10.1115/1.3445549 | |
journal fristpage | 177 | |
journal lastpage | 182 | |
identifier eissn | 0742-4795 | |
keywords | Heat transfer | |
keywords | Machinery | |
keywords | Clearances (Engineering) | |
keywords | Cylinders | |
keywords | Fourier series | |
keywords | Wall thickness | |
keywords | Temperature gradients | |
keywords | Motion | |
keywords | Electrical resistance | |
keywords | Gas flow | |
keywords | Thermal diffusivity AND Materials properties | |
tree | Journal of Engineering for Gas Turbines and Power:;1971:;volume( 093 ):;issue: 002 | |
contenttype | Fulltext |