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  • FLUID MECHANICS AND HEAT TRANSFER  (19)
  • (9E)-2,6,10,14-Tetramethyl-7-(3-methylpent-4-enyliden)pentadeca-9-ene per unit sediment mass; (9Z)-2,6,10,14-Tetramethyl-7-(3-methylpent-4-enyliden)pentadeca-9-ene per unit sediment mass; 2,10,14-Trimethyl-6-enyl-7-(3-methylpent-1-enyl)pentadecene per unit sediment mass; 2,6,10,14-Tetramethyl-7-(3-methylpent-4-enyl)pentadecane per unit sediment mass; 24-Ethylcholest-5-en-3beta-ol, fraction; 24-Methylcholest-5-en-3beta-ol, fraction; 24-Methylcholesta-5,22E-dien-3beta-ol per unit sediment mass; 323-U1343; AGE; Bering Sea; Bering Sea Paleoceanography; Bulimina exilis; Cassidulinoides parkeriana; Cholesterol, fraction; Classification; COMPCORE; Composite Core; Counting; DEPTH, sediment/rock; Elphidium batialis; Epistominella pulchella; Exp323; Foraminifera, benthic, other; Foraminifera, benthic, total; Gas chromatography - Mass spectrometry (GC-MS); Globobulimina spp.; Integrated Ocean Drilling Program / International Ocean Discovery Program; IODP; Islandiella norcrossi; Joides Resolution; Magnesium/Calcium ratio; Manganese/Calcium ratio; Nonionella digitata; Nonionella labradorica; Phytoplankton biomarker Brassicasterol IP25 index; Phytoplankton biomarker C25 HBI (Z) triene IP25 index; Species; Uranium/Calcium ratio; Uranium/Manganese ratio; Uvigerina spp.; Valvulineria araucana  (1)
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  • 11
    Publication Date: 2019-06-28
    Description: The effects of streamwise convex curvature, recovery, and freestream turbulence intensity on the turbulent transport of heat and momentum in a mature boundary layer are studied using a specially designed three-wire hot-wire probe. Increased freestream turbulence is found to increase the profiles throughout the boundary layer on the flat developing wall. Curvature effects were found to dominate turbulence intensity effects for the present cases considered. For the higher TI (turbulence intensity) case, negative values of the turbulent Prandtl number are found in the outer half of the boundary layer, indicating a breakdown in Reynolds analogy.
    Keywords: FLUID MECHANICS AND HEAT TRANSFER
    Type: ASME PAPER 87-GT-199
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  • 12
    Publication Date: 2019-07-13
    Description: Surface heat transfer rates have been measured for several different flows on an isothermal, convexly curved surface. The freestream velocity, boundary layer thickness, acceleration parameter, and unheated starting length were varied systematically, and both turbulent and transitional boundary layers were studied. The effect of convex curvature on heat transfer rates is significant with Stanton numbers reduced 20-25% below flat wall values for the same enthalpy thickness Reynolds number. Heat transfer rates recovered slowly on a flat wall downstream of the curved wall, and after 60 cm, the Stanton numbers were still 15-20% below flat wall values. The behavior of the boundary layer suggests the existence of an asymptotic condition. Boundary layer thickness, freestream velocity, and boundary layer maturity affect the initial response to the introduction of curvature and the rate at which the asymptotic state is approached. Convex curvature appears to increase the boundary layer's sensitivity to acceleration; it also delays and retards transition. Near-laminar or early-transitional boundary layers recover from curvature rapidly, whereas late-transitional and mature boundary layers recover slowly.
    Keywords: FLUID MECHANICS AND HEAT TRANSFER
    Type: ASME PAPER 81-HT-78 , American Society of Mechanical Engineers and American Institute of Chemical Engineers, National Heat Transfer Conference; Aug 02, 1981 - Aug 05, 1981; Milwaukee, WI
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  • 13
    Publication Date: 2019-07-13
    Description: Measurements have been made of the heat transfer through a turbulent boundary layer on a convexly curved isothermal wall and on a flat plate following the curved section. Data were taken for one free-stream velocity and two different ratios of boundary layer thickness to radius of curvature delta/R = 0.051 and delta/R = 0.077. Only small differences were observed in the distribution of heat transfer rates for the two boundary layer thicknesses tested, although differences were noted in the temperature distributions within the boundary layer
    Keywords: FLUID MECHANICS AND HEAT TRANSFER
    Type: ASME PAPER 79-WA/GT-10 , Winter Annual Meeting; Dec 02, 1979 - Dec 07, 1979; New York, NY
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  • 14
    Publication Date: 2019-07-13
    Description: A convexly curved and isothermally heated wall with a 45-cm radius of curvature is subjected to turbulent boundary layer flow measurements in order to determine wall heat transfer rates and mean velocity and temperature profiles. Significant curvature effects are noted, with Stanton number and skin friction coefficient reductions of 35-40 percent by comparison with flat plate values for the same momentum or enthalpy thickness Reynolds numbers. Profiles of mean velocity and temperature show a more rapid growth of the wake regions, and a shortening of the log-linear region, as a result of curvature. Turbulent Prandtl numbers deduced from the mean temperature profiles under the assumption of a wall thermal law were found to be increased by 40-50 percent by this strong convex curvature.
    Keywords: FLUID MECHANICS AND HEAT TRANSFER
    Type: Heat transfer 1982; Sep 06, 1982 - Sep 10, 1982; Munich
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  • 15
    Publication Date: 2019-07-12
    Keywords: FLUID MECHANICS AND HEAT TRANSFER
    Type: Journal of Thermophysics and Heat Transfer (ISSN 0887-8722); 3; 19-26
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  • 16
    Publication Date: 2019-07-13
    Description: To improve the prediction of Stirling engine performance, a more realistic model of oscillating flow losses in tubular heat exchangers is necessary. An experimental investigation has therefore been initiated to determine the effects of flow oscillation on fluid mechanics and heat transfer in ducts. This paper presents the first velocity measurements taken in this investigation.
    Keywords: FLUID MECHANICS AND HEAT TRANSFER
    Type: 1988 IECEC; Jul 31, 1988 - Aug 05, 1988; Denver, CO; United States
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  • 17
    Publication Date: 2019-07-13
    Description: Hot-wire anemometry techniques used to document laminar-to-turbulent transition in oscillating flow are discussed, and two transition mechanisms proposed by Seume (1988) are reviewed. Reliable near-wall data, and the convergence of ensemble-averaged velocities and rms velocity fluctuations will aid in evaluating wall shear stresses and calculating various boundary-layer parameters. Special consideration was given to a detailed measurement program which documents transition at different axial positions for the space power research engine (SPRE) operating point. Future work on the effect of entry geometry and measurements of heat transfer are outlined. In order to better simulate flow conditions in actual Stirling engine heat exchangers, the effects of various inflow geometries are investigated. Once the hydrodynamic conditions in the test section are documented, a measurement program to assess the effect of flow oscillation on heat transfer will commence.
    Keywords: FLUID MECHANICS AND HEAT TRANSFER
    Type: Intersociety Energy Conversion Engineering Conference; Aug 12, 1990 - Aug 17, 1990; Reno, NV; United States
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  • 18
    Publication Date: 2019-07-12
    Description: The test section of the present experiment to ascertain the effects of convex curvature and freestream turbulence on boundary layer momentum and heat transfer during natural transition provided a two-dimensional boundary layer flow on a uniformly heated curved surface, with bending to various curvature radii, R. Attention is given to results for the cases of R = infinity, 180 cm, and 90 cm, each with two freestream turbulence intensity levels. While the mild convex curvature of R = 180 cm delays transition, further bending to R = 90 cm leads to no signifucant further delay of transition. Cases with both curvature and higher freestream disturbance effects exhibit the latter's pronounced dominance. These data are pertinent to the development of transition prediction models for gas turbine blade design.
    Keywords: FLUID MECHANICS AND HEAT TRANSFER
    Type: ASME PAPER 85-MT-60 , ASME, Transactions, Journal of Turbomachinery (ISSN 0889-504X); 109; 443-452
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  • 19
    Publication Date: 2019-07-13
    Description: A description of the University of Minnesota Oscillating Flow Test Program is presented. The rationale for isolating the oscillating flow effect for separate study, the objectives of the test program, and the program design criteria are presented along with a description of the test facility and the test plan. The program test domain covers almost the entire operating domain of Stirling engine heat exchangers expressed in terms of the appropriate dimensionless parameters. Phenomena important to Stirling engine performance which are not simulated in the test program are also discussed. Computer analysis results are used to predict apparatus performance.
    Keywords: FLUID MECHANICS AND HEAT TRANSFER
    Type: IECEC ''87; Aug 10, 1987 - Aug 14, 1987; Philadelphia, PA; United States
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  • 20
    Publication Date: 2019-07-12
    Description: Experimental results are presented to document hydrodynamic and thermal development of flat-plate boundary layers undergoing natural transition. Local heat transfer coefficients, skin friction coefficients and profiles of velocity, temperature and Reynolds normal and shear stresses are presented. A case with no transition and transitional cases with 0.68 percent and 2.0 percent free-stream disturbance intensities were investigated. The locations of transition are consistent with earlier data. A late-laminar state with significant levels of turbulence is documented. In late-transitional and early-turbulent flows, turbulent Prandtl number and conduction layer thickness values exceed, and the Reynolds analogy factor is less than, values previously measured in fully turbulent flows.
    Keywords: FLUID MECHANICS AND HEAT TRANSFER
    Type: ASME PAPER 85-GT-113 , ASME, Transactions, Journal of Engineering for Gas Turbines and Power (ISSN 0022-0825); 107; 1007-101
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