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    The Problem of Pneumatic Pressure Lag: Part 1—Steady-State Flow in a Tubing System

    Source: Journal of Fluids Engineering:;1964:;volume( 086 ):;issue: 002::page 234
    Author:
    A. L. Ducoffe
    ,
    F. M. White
    DOI: 10.1115/1.3653045
    Publisher: The American Society of Mechanical Engineers (ASME)
    Abstract: An analytical and experimental investigation of the steady-state isothermal flow in a series system, comprised of a constant-diameter tube with reduced size unions located at the tube extremities, is reported herein. The pressure drop across the system has been determined experimentally as a function of the system geometry. The parameters chosen for investigation were the tube length to diameter ratio L/D, the union diameter to tube diameter ratio Df /D, and the Reynolds number. The ranges of the parameters investigated consisted of 159 ≤ L/D ≤ 1475, 0.7 ≤ Df /D ≤ 1.0, and 200 ≤ Reynolds number ≤ 100,000. All tests were conducted at room temperature. The theory is derived considering each geometric element of the system, such as inlet, development length, exit, and so on, and a set of five simultaneous algebraic flow equations results. Solutions to these were obtained by use of a digital computer. A pseudo-friction factor, for fully developed laminar or turbulent flow, is defined. The result indicates that the correlation of theory with experiment is quantitative over the range of parameters investigated.
    keyword(s): Pressure , Flow (Dynamics) , Tubing , Steady state , Reynolds number , Computers , Equations , Geometry , Pressure drop , Friction , Temperature AND Turbulence ,
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      The Problem of Pneumatic Pressure Lag: Part 1—Steady-State Flow in a Tubing System

    URI
    http://yetl.yabesh.ir/yetl1/handle/yetl/101435
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    • Journal of Fluids Engineering

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    contributor authorA. L. Ducoffe
    contributor authorF. M. White
    date accessioned2017-05-08T23:23:01Z
    date available2017-05-08T23:23:01Z
    date copyrightJune, 1964
    date issued1964
    identifier issn0098-2202
    identifier otherJFEGA4-27254#234_1.pdf
    identifier urihttp://yetl.yabesh.ir/yetl/handle/yetl/101435
    description abstractAn analytical and experimental investigation of the steady-state isothermal flow in a series system, comprised of a constant-diameter tube with reduced size unions located at the tube extremities, is reported herein. The pressure drop across the system has been determined experimentally as a function of the system geometry. The parameters chosen for investigation were the tube length to diameter ratio L/D, the union diameter to tube diameter ratio Df /D, and the Reynolds number. The ranges of the parameters investigated consisted of 159 ≤ L/D ≤ 1475, 0.7 ≤ Df /D ≤ 1.0, and 200 ≤ Reynolds number ≤ 100,000. All tests were conducted at room temperature. The theory is derived considering each geometric element of the system, such as inlet, development length, exit, and so on, and a set of five simultaneous algebraic flow equations results. Solutions to these were obtained by use of a digital computer. A pseudo-friction factor, for fully developed laminar or turbulent flow, is defined. The result indicates that the correlation of theory with experiment is quantitative over the range of parameters investigated.
    publisherThe American Society of Mechanical Engineers (ASME)
    titleThe Problem of Pneumatic Pressure Lag: Part 1—Steady-State Flow in a Tubing System
    typeJournal Paper
    journal volume86
    journal issue2
    journal titleJournal of Fluids Engineering
    identifier doi10.1115/1.3653045
    journal fristpage234
    journal lastpage240
    identifier eissn1528-901X
    keywordsPressure
    keywordsFlow (Dynamics)
    keywordsTubing
    keywordsSteady state
    keywordsReynolds number
    keywordsComputers
    keywordsEquations
    keywordsGeometry
    keywordsPressure drop
    keywordsFriction
    keywordsTemperature AND Turbulence
    treeJournal of Fluids Engineering:;1964:;volume( 086 ):;issue: 002
    contenttypeFulltext
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    DSpace software copyright © 2002-2015  DuraSpace
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