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  • Author > Lin, Chin-Shun [x]

  • Sort results by: NASA Center | Date Added to NTRS | Publication Year
    There are a total of 13 record(s) matching your query.
    Sorted by: Date Added To NTRS in Descending order

    1 2 Next 
    Numerical calculations of turbulent reacting flow in a gas-turbine combustor

    Author(s): Lin, Chin-Shun
    Abstract: A numerical study for confined, axisymmetrical, turbulent diffusion flames is presented. Local mean gas properties are predicted by solving the appropriate conservation equations in the finite difference form with the ...
    NASA Center: Glenn Research Center
    Publication Year: 1987
    Added to NTRS: 2005-10-13
    Accession Number: 87N20171; Document ID: 19870010738; Report Number: E-3501, ICOMP-87-2, NAS 1.15:89842, NASA-TM-89842

    Buoyancy effects on the vapor condensation rate on a horizontal liquid surface

    Author(s): Hasan, Mohammad M.; Lin, Chin-Shun
    Abstract: The results are presented of a numerical study of the effects of buoyancy on the direct condensation of saturated or nearly saturated vapor on a horizontal liquid surface in a cylindrical tank. The liquid motion beneath the ...
    NASA Center: Glenn Research Center
    Publication Year: 1989
    Added to NTRS: 2005-08-25
    Accession Number: 90N13675; Document ID: 19900004359; Report Number: AIAA PAPER 90-0353, E-5206, NAS 1.15:102437, NASA-TM-102437

    Axisymmetric confined turbulent jet directed towards the liquid surface from below

    Author(s): Hasan, Mohammad M.; Lin, Chin-Shun
    Abstract: A numerical simulation is presented of an axisymmetric turbulent jet discharging axially from below into a cylindrical tank and directed towards the liquid vapor interface. The liquid vapor interface is assumed to be flat ...
    NASA Center: Glenn Research Center
    Publication Year: 1988
    Added to NTRS: 2005-08-25
    Accession Number: 89N13749; Document ID: 19890004378; Report Number: AIAA PAPER 89-0172, E-4499, NAS 1.15:101409, NASA-TM-101409

    Numerical studies of the effects of jet-induced mixing on liquid-vapor interface condensation

    Author(s): Lin, Chin-Shun
    Abstract: Numerical solutions of jet-induced mixing in a partially full cryogenic tank are presented. An axisymmetric laminar jet is discharged from the central part of the tank bottom toward the liquid-vapor interface. Liquid is ...
    NASA Center: NASA (non Center Specific)
    Publication Year: 1989
    Added to NTRS: 2005-08-25
    Accession Number: 89N23818; Document ID: 19890014447; Report Number: AIAA PAPER 89-1744, E-4749, NAS 1.26:182285, NASA-CR-182285

    Similar solutions for viscous hypersonic flow over a slender three-fourths-power body of revolution

    Author(s): Lin, Chin-Shun
    Abstract: For hypersonic flow with a shock wave, there is a similar solution consistent throughout the viscous and inviscid layers along a very slender three-fourths-power body of revolution The strong pressure interaction problem can ...
    NASA Center: Glenn Research Center
    Publication Year: 1987
    Added to NTRS: 2005-08-25
    Accession Number: 88N12752; Document ID: 19880003370; Report Number: E-3803, ICOMP-87-7, NAS 1.15:100205, NASA-TM-100205

    Numerical investigation of the thermal stratification in cryogenic tanks subjected to wall heat flux

    Author(s): Lin, Chin-Shun; Hasan, Mohammad H.
    Abstract: The flow pattern and thermal stratification of a cryogenic cylindrical tank are numerically studied. The tank sidewall is subjected to either a uniform heat-flux or two discrete levels of uniform heat-flux at the upper and ...
    NASA Center: Glenn Research Center
    Publication Year: 1990
    Added to NTRS: 2005-08-25
    Accession Number: 90N27984; Document ID: 19900018668; Report Number: AIAA PAPER 90-2375, E-5545, NAS 1.15:103194, NASA-TM-103194

    Vapor condensation on liquid surface due to laminar jet-induced mixing: The effects of system parameters

    Author(s): Lin, Chin-Shun; Hasan, Mohammad M.
    Abstract: The effects of system parameters on the interface condensation rate in a laminar jet induced mixing tank are numerically studied. The physical system consists of a partially filled cylindrical tank with a slightly subcooled ...
    NASA Center: Glenn Research Center
    Publication Year: 1989
    Added to NTRS: 2005-08-25
    Accession Number: 90N13751; Document ID: 19900004435; Report Number: AIAA PAPER 90-0354, E-5201, NAS 1.15:102433, NASA-TM-102433

    Buoyancy effects on the vapor condensation rate on a horizontal liquid surface

    Author(s): Hasan, Mohammad M.; Lin, Chin-Shun
    Abstract: The results are presented of a numerical study of the effects of buoyancy on the direct condensation of saturated or nearly saturated vapor on a horizontal liquid surface in a cylindrical tank. The liquid motion beneath the ...
    NASA Center: Glenn Research Center
    Publication Year: 1990
    Added to NTRS: 2004-11-03
    Accession Number: 90A22201; Document ID: 19900035146; Report Number: AIAA PAPER 90-0353

    Numerical investigation of the thermal stratification in cryogenic tanks subjected to wall heat flux

    Author(s): Lin, Chin-Shun; Hasan, Mohammed M.
    Abstract: The flow pattern and thermal stratification of a cryogenic cylindrical tank are numerically studied. The tank sidewall is subjected to either a uniform heat-flux or two discrete levels of uniform heat-flux at the upper and ...
    NASA Center: Glenn Research Center
    Publication Year: 1990
    Added to NTRS: 2004-11-03
    Accession Number: 90A52500; Document ID: 19900065445; Report Number: AIAA PAPER 90-2375

    Numerical studies of the effects of jet-induced mixing on liquid-vapor interface condensation

    Author(s): Lin, Chin-Shun
    Abstract: Numerical solutions of jet-induced mixing in a partially full cryogenic tank are presented. An axisymmetric laminar jet is discharged from the central part of the tank bottom toward the liquid-vapor interface. Liquid is ...
    NASA Center: Glenn Research Center
    Publication Year: 1989
    Added to NTRS: 2004-11-03
    Accession Number: 89A48958; Document ID: 19890061587; Report Number: AIAA PAPER 89-1744

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