SUPERCOMPUTATIONS of LOW-PRANDTL-NUMBER CONVECTION FLOWS Jorg¨ Schumacher1 and Janet D

Total Page:16

File Type:pdf, Size:1020Kb

SUPERCOMPUTATIONS of LOW-PRANDTL-NUMBER CONVECTION FLOWS Jorg¨ Schumacher1 and Janet D XXIV ICTAM, 21-26 August 2016, Montreal, Canada SUPERCOMPUTATIONS OF LOW-PRANDTL-NUMBER CONVECTION FLOWS Jorg¨ Schumacher1 and Janet D. Scheel2 1Department of Mechanical Engineering, Technische Universitat¨ Ilmenau, Ilmenau, Germany 2Department of Physics, Occidental College, Los Angeles, USA Summary Massively parallel supercomputations are an important analysis tool to study the fundamental local and global mechanisms of heat and momentum transfer in turbulent convection. We discuss the perspectives and challenges in this vital field of fundamental turbulence research for the case of convection at very low Prandtl numbers. MOTIVATION AND SIMULATION MODEL Turbulent convection is an important area of present research in fluid dynamics with applications to diverse phenomena in nature and technology. The turbulent Rayleigh-Benard´ convection (RBC) model is at the core of all these turbulent flows. It can be studied in a controlled manner, but has enough complexity to contain the key features of turbulence in heated fluids. This flow in cylindrical cells has been investigated intensively over the last few years in several laboratory experiments all over the world [1]. In RBC, a fluid cell or layer is kept at a constant temperature difference ∆T = Tbottom − Ttop between top and bottom plates which are separated by a vertical distance H. The Rayleigh and Prandtl numbers are given by gαH3∆T ν Ra = and P r = : (1) νκ κ The parameter Ra characterizes the thermal driving in convective turbulence with the acceleration due to gravity, g, the thermal expansion coefficient, α, the kinematic viscosity, ν, and the thermal diffusivity, κ. The hard turbulence regime in RBC is established for Ra ≥ 106. The Prandtl number P r characterizes the molecular properties the working fluid. The aspect ratio Γ, which is the ratio of cell diameter or cell length and cell height H, is the third input parameter. In this contribution, we will focus on the specific turbulence properties of convection at very low Prandtl numbers and the resulting challenges for supercomputer simulations. The three-dimensional Boussinesq equations (2)–(4) are used to model Rayleigh-Benard´ convection. They are given in dimensionless form by r · u = 0 ; (2) r @u P r + (u · r)u = −∇p + r2u + T e ; (3) @t Ra z @T 1 + (u · r)T = p r2T: (4) @t RaP r The variable u(r; t) is the velocity field, p(r; t) is the pressure, and T (r; t) is the temperature. We use no-slip velocity boundary conditions along all walls of the closed cylindrical cell. The temperature field obeys insulating sidewalls and constant values along the top and bottom plates. A spectral element method (SEM) is applied which is based on the Nek5000 software package [2]. The order of the Lagrangian interpolation polynomials for the expansion on each element (see the element mesh in the left panel of figure 1) which is used in each space direction is as high as N − 1 = 13. This code is a pure MPI code which scales very well up to ∼ 106 MPI tasks. Numerical details and comprehensive resolution tests are found in Scheel et al. [3]. The SEM is preferred if the fine-scale structure, i.e. gradients of the turbulent fields have to be analyzed. TURBULENT CONVECTION AT VERY LOW PRANDTL NUMBERS Compared to the vast number of investigations of turbulent convection in air or water, the very-low-P r regime appears almost as a “Terra incognita” despite many applications. Turbulent convection in the Sun is present at Prandtl numbers P r < 10−3, in the liquid metal core of the Earth one finds P r ∼ 10−2. Convection flows as present in material processing, nuclear engineering, or liquid metal batteries have Prandtl numbers between 5×10−3 and 2×10−2. One reason for significantly fewer studies of convection at low Prandtl numbers is that laboratory measurements have to be conducted in opaque and aggressive liquid metals when P r should become much smaller than 0.1. Direct numerical simulations (DNS) are currently the only way to gain access to the full three-dimensional convective turbulent fields in low-P r convection. However, these simulations become very demanding when the small-scale structure of turbulence has to be studied, even for moderate Rayleigh numbers Ra. To give an example: a simulation for convection Figure 1: Left: Spectral element grid for the RBC cell. Right: Snapshot of the dynamics in the vicinity of the bottom plate of the convection cell. We show field lines of the wall shear stress field and isocontours of the magnitude of the wall-normal vorticity component. The snapshot is for convection in liquid mercury at P r = 0:021 at Ra = 108. in liquid sodium at Ra = 2:38 × 106 and P r = 0:005 required the same SEM mesh of 4:1 × 109 cells as a simulation for convection in air at Ra = 1010 and P r = 0:7. The latter Rayleigh number is almost four orders of magnitude larger than in sodium. Both runs were conducted with 65,536 MPI tasks on BG/Q. What makes these simulations so expensive? While the heat transport is reduced in low–P r convection, the production of vorticity and shear are enhanced significantly. We found that this in turn amplifies the small-scale intermittency in these flows and makes them more comparable to classical Kolmogorov turbulence [4]. We have also shown in [4] that the cascade of the fluid turbulence is extended at the large-scale and small-scale end with decreasing Prandtl number thus enhancing the flow Reynolds number and consequently the turbulent momentum transport in the convection flow. The more vigorous fluid turbulence enhances in the enstrophy production in the fluid. Since the Rayleigh-Benard´ fluid is confined, tiny boundary layers of the temperature and velocity fields form in the vicinity of the walls. Figure 1 (right) displays a snapshot of the velocity boundary layer dynamics at the bottom plate for our biggest simulation in liquid mercury with 131,072 MPI tasks on BG/Q. This figure and our comprehensive analysis suggest that turbulence is also strongly amplified in the boundary layers although the Rayleigh number seems to be moderate. An increase from the present value of Ra = 108 to Ra = 5 × 108 requires 1:3 × 1010 mesh cells and 524,288 MPI tasks for a well-resolved run. We will also discuss the increasing challenges in the data analysis which one faces for these big simulations. Our research topic demonstrates clearly that supercomputing has become an essential tool for revealing the secrets of turbulence, and especially those of turbulent convection. ACKNOWLEDGEMENTS The work of JS is supported by the Deutsche Forschungsgemeinschaft. We want to thank the John von Neumann-Institute for Computing for the support with supercomputing resources by projects HIL07 and HIL09 as well as the Scientific Big Data Analytics Project SBDA003. This work is also supported by the DOE INCITE projects RayBen (2014) and LiquidGaNa (2016). References [1] Chilla` F. and Schumacher J.: New perspectives in turbulent Rayleigh-Benard´ convection. Eur. J. Phys. E 35: no. 58, 2012. [2] Nek5000 Website: https://www.nek5000.mcs.anl.gov/ [3] Scheel J. D., Emran M. S. and Schumacher J.: Resolving the fine-scale structure in turbulent Rayleigh-Benard´ convection. New J. Phys. 15: no. 113063, 2013. [4] Schumacher J., Gotzfried¨ P. and Scheel J. D.: Enhanced enstrophy generation for turbulent convection in low–Prandtl number fluids. Proc. Natl. Acad. Sci. USA 112: 9530–9535, 2015..
Recommended publications
  • Convection Heat Transfer
    Convection Heat Transfer Heat transfer from a solid to the surrounding fluid Consider fluid motion Recall flow of water in a pipe Thermal Boundary Layer • A temperature profile similar to velocity profile. Temperature of pipe surface is kept constant. At the end of the thermal entry region, the boundary layer extends to the center of the pipe. Therefore, two boundary layers: hydrodynamic boundary layer and a thermal boundary layer. Analytical treatment is beyond the scope of this course. Instead we will use an empirical approach. Drawback of empirical approach: need to collect large amount of data. Reynolds Number: Nusselt Number: it is the dimensionless form of convective heat transfer coefficient. Consider a layer of fluid as shown If the fluid is stationary, then And Dividing Replacing l with a more general term for dimension, called the characteristic dimension, dc, we get hd N ≡ c Nu k Nusselt number is the enhancement in the rate of heat transfer caused by convection over the conduction mode. If NNu =1, then there is no improvement of heat transfer by convection over conduction. On the other hand, if NNu =10, then rate of convective heat transfer is 10 times the rate of heat transfer if the fluid was stagnant. Prandtl Number: It describes the thickness of the hydrodynamic boundary layer compared with the thermal boundary layer. It is the ratio between the molecular diffusivity of momentum to the molecular diffusivity of heat. kinematic viscosity υ N == Pr thermal diffusivity α μcp N = Pr k If NPr =1 then the thickness of the hydrodynamic and thermal boundary layers will be the same.
    [Show full text]
  • Turbulent-Prandtl-Number.Pdf
    Atmospheric Research 216 (2019) 86–105 Contents lists available at ScienceDirect Atmospheric Research journal homepage: www.elsevier.com/locate/atmosres Invited review article Turbulent Prandtl number in the atmospheric boundary layer - where are we T now? ⁎ Dan Li Department of Earth and Environment, Boston University, Boston, MA 02215, USA ARTICLE INFO ABSTRACT Keywords: First-order turbulence closure schemes continue to be work-horse models for weather and climate simulations. Atmospheric boundary layer The turbulent Prandtl number, which represents the dissimilarity between turbulent transport of momentum and Cospectral budget model heat, is a key parameter in such schemes. This paper reviews recent advances in our understanding and modeling Thermal stratification of the turbulent Prandtl number in high-Reynolds number and thermally stratified atmospheric boundary layer Turbulent Prandtl number (ABL) flows. Multiple lines of evidence suggest that there are strong linkages between the mean flowproperties such as the turbulent Prandtl number in the atmospheric surface layer (ASL) and the energy spectra in the inertial subrange governed by the Kolmogorov theory. Such linkages are formalized by a recently developed cospectral budget model, which provides a unifying framework for the turbulent Prandtl number in the ASL. The model demonstrates that the stability-dependence of the turbulent Prandtl number can be essentially captured with only two phenomenological constants. The model further explains the stability- and scale-dependences
    [Show full text]
  • Chapter 5 Dimensional Analysis and Similarity
    Chapter 5 Dimensional Analysis and Similarity Motivation. In this chapter we discuss the planning, presentation, and interpretation of experimental data. We shall try to convince you that such data are best presented in dimensionless form. Experiments which might result in tables of output, or even mul- tiple volumes of tables, might be reduced to a single set of curves—or even a single curve—when suitably nondimensionalized. The technique for doing this is dimensional analysis. Chapter 3 presented gross control-volume balances of mass, momentum, and en- ergy which led to estimates of global parameters: mass flow, force, torque, total heat transfer. Chapter 4 presented infinitesimal balances which led to the basic partial dif- ferential equations of fluid flow and some particular solutions. These two chapters cov- ered analytical techniques, which are limited to fairly simple geometries and well- defined boundary conditions. Probably one-third of fluid-flow problems can be attacked in this analytical or theoretical manner. The other two-thirds of all fluid problems are too complex, both geometrically and physically, to be solved analytically. They must be tested by experiment. Their behav- ior is reported as experimental data. Such data are much more useful if they are ex- pressed in compact, economic form. Graphs are especially useful, since tabulated data cannot be absorbed, nor can the trends and rates of change be observed, by most en- gineering eyes. These are the motivations for dimensional analysis. The technique is traditional in fluid mechanics and is useful in all engineering and physical sciences, with notable uses also seen in the biological and social sciences.
    [Show full text]
  • Turbulent Prandtl Number and Its Use in Prediction of Heat Transfer Coefficient for Liquids
    Nahrain University, College of Engineering Journal (NUCEJ) Vol.10, No.1, 2007 pp.53-64 Basim O. Hasan Chemistry. Engineering Dept.- Nahrain University Turbulent Prandtl Number and its Use in Prediction of Heat Transfer Coefficient for Liquids Basim O. Hasan, Ph.D Abstract: eddy conductivity is unspecified in the case of heat transfer. The classical approach for obtaining the A theoretical study is performed to determine the transport mechanism for the heat transfer problem turbulent Prandtl number (Prt ) for liquids of wide follows the laminar approach, namely, the momentum range of molecular Prandtl number (Pr=1 to 600) and thermal transport mechanisms are related by a under turbulent flow conditions of Reynolds number factor, the Prandtl number, hence combining the range 10000- 100000 by analysis of experimental molecular and eddy viscosities one obtain the momentum and heat transfer data of other authors. A Boussinesq relation for shear stress: semi empirical correlation for Prt is obtained and employed to predict the heat transfer coefficient for du the investigated range of Re and molecular Prandtl ( ) 1 number (Pr). Also an expression for momentum eddy m dy diffusivity is developed. The results revealed that the Prt is less than 0.7 and is function of both Re and Pr according to the following relation: and the analogous relation for heat flux: Prt=6.374Re-0.238 Pr-0.161 q dT The capability of many previously proposed models of ( h ) 2 Prt in predicting the heat transfer coefficient is c p dy examined. Cebeci [1973] model is found to give good The turbulent Prandtl number is the ratio between the accuracy when used with the momentum eddy momentum and thermal eddy diffusivities, i.e., Prt= m/ diffusivity developed in the present analysis.
    [Show full text]
  • Anomalous Viscosity, Resistivity, and Thermal Diffusivity of the Solar
    Anomalous Viscosity, Resistivity, and Thermal Diffusivity of the Solar Wind Plasma Mahendra K. Verma Department of Physics, Indian Institute of Technology, Kanpur 208016, India November 12, 2018 Abstract In this paper we have estimated typical anomalous viscosity, re- sistivity, and thermal difffusivity of the solar wind plasma. Since the solar wind is collsionless plasma, we have assumed that the dissipation in the solar wind occurs at proton gyro radius through wave-particle interactions. Using this dissipation length-scale and the dissipation rates calculated using MHD turbulence phenomenology [Verma et al., 1995a], we estimate the viscosity and proton thermal diffusivity. The resistivity and electron’s thermal diffusivity have also been estimated. We find that all our transport quantities are several orders of mag- nitude higher than those calculated earlier using classical transport theories of Braginskii. In this paper we have also estimated the eddy turbulent viscosity. arXiv:chao-dyn/9509002v1 5 Sep 1995 1 1 Introduction The solar wind is a collisionless plasma; the distance travelled by protons between two consecutive Coulomb collisions is approximately 3 AU [Barnes, 1979]. Therefore, the dissipation in the solar wind involves wave-particle interactions rather than particle-particle collisions. For the observational evidence of the wave-particle interactions in the solar wind refer to the review articles by Gurnett [1991], Marsch [1991] and references therein. Due to these reasons for the calculations of transport coefficients in the solar wind, the scales of wave-particle interactions appear more appropriate than those of particle-particle interactions [Braginskii, 1965]. Note that the viscosity in a turbulent fluid is scale dependent.
    [Show full text]
  • Prandtl Number and Thermoacoustic Refrigerators M
    Prandtl number and thermoacoustic refrigerators M. E. H. Tijani, J. C. H. Zeegers, and A. T. A. M. de Waele Department of Applied Physics, Eindhoven University of Technology, P.O. Box 513, 5600 MB Eindhoven, The Netherlands ͑Received 28 November 2001; revised 25 April 2002; accepted 4 May 2002͒ From kinetic gas theory, it is known that the Prandtl number for hard-sphere monatomic gases is 2/3. Lower values can be realized using gas mixtures of heavy and light monatomic gases. Prandtl numbers varying between 0.2 and 0.67 are obtained by using gas mixtures of helium–argon, helium–krypton, and helium–xenon. This paper presents the results of an experimental investigation into the effect of Prandtl number on the performance of a thermoacoustic refrigerator using gas mixtures. The measurements show that the performance of the refrigerator improves as the Prandtl number decreases. The lowest Prandtl number of 0.2, obtained with a mixture containing 30% xenon, leads to a coefficient of performance relative to Carnot which is 70% higher than with pure helium. © 2002 Acoustical Society of America. ͓DOI: 10.1121/1.1489451͔ PACS numbers: 43.35.Ud, 43.35.Ty ͓RR͔ I. INTRODUCTION while compressing and expanding. The interaction of the moving gas in the stack with the stack surface generates heat The basic understanding of the physical principles un- transport.2 A detailed description of the refrigerator can be derlying the thermoacoustic effect is well established and has found in the literature.3,6 been discussed in many papers.1,2 However, a quantitative experimental investigation of the effect of some important parameters on the behavior of the thermoacoustic devices is II.
    [Show full text]
  • Numerical Calculations of Two-Dimensional Large Prandtl Number Convection in a Box
    J. Fluid Mech. (2013), vol. 729, pp. 584–602. c Cambridge University Press 2013 584 doi:10.1017/jfm.2013.330 Numerical calculations of two-dimensional large Prandtl number convection in a box J. A. Whitehead1,†, A. Cotel2, S. Hart3, C. Lithgow-Bertelloni4 and W. Newsome5 1Physical Oceanography Department, Woods Hole Oceanographic Institution, Woods Hole, MA 02543, USA 2Civil and Environmental Engineering Department, University of Michigan, 1351 Beal Avenue, Ann Arbor, MI 48109, USA 3Geology and Geophysics Department, Woods Hole Oceanographic Institution, Woods Hole, MA 02543, USA 4Department of Earth Sciences, University College London, Gower Street, London WC1E 6BT, UK 5Geological Sciences Department, University of Michigan, 1100 North University Avenue, Ann Arbor, MI 48109, USA (Received 30 August 2012; revised 17 June 2013; accepted 22 June 2013; first published online 24 July 2013) Convection from an isolated heat source in a chamber has been previously studied numerically, experimentally and analytically. These have not covered long time spans for wide ranges of Rayleigh number Ra and Prandtl number Pr. Numerical calculations of constant viscosity convection partially fill the gap in the ranges Ra 103–106 and Pr 1; 10; 100; 1000 and . Calculations begin with cold fluid everywhereD and localizedD hot temperature at1 the centre of the bottom of a square two-dimensional chamber. For Ra > 20 000, temperature increases above the hot bottom and forms a rising plume head. The head has small internal recirculation and minor outward conduction of heat during ascent. The head approaches the top, flattens, splits and the two remnants are swept to the sidewalls and diffused away.
    [Show full text]
  • The Influence of Prandtl Number on Free Convection in a Rectangular Cavity
    hr. J. Heor Mm\ Transfer. Vol. 24, pp. 125-131 0017-93lO/8ljOlOl-0125SOsoZ.OO/O 0 Pergamon Press Ltd. 1981. Printed in GreatBritain THE INFLUENCE OF PRANDTL NUMBER ON FREE CONVECTION IN A RECTANGULAR CAVITY W. P. GRAEBEL Department of Mechanical Engineering and Applied Mechanics, The University of Michigan, Ann Arbor, MI. 48109, U.S.A. (Receioed 19 May 1980) Abstract-Natural convection in a rectangular cavity is considered for the problem where one vertical wall is heated and the other is cooled. The boundary layer flow is solved using a modified Oseen technique in a manner similar to Gill’s solution. Temperature and velocity profiles in the core, and the Nusselt number, are found as functions of the Rayleigh and Prandtl numbers and the length ratio. The solution indicates that for a Prandtl number less than l/7, a midsection shear layer develops. NOMENCLATURE more reasonable matching condition and obtained overall Nusselt numbers which are in good agreement C, constant of integration; with available experimental and numerical heat- 9, gravitational constant ; transfer data. H, cavity height; The present note generalizes Gill’s results for arbit- K = (Pr - l)/(Pr + 1); rary values of the Prandtl number, so that the small L, cavity length; Prandtl number limit, suitable for liquid metals, can Nu, Nusselt number ; pressure; also be obtained. The method of Bejan is used in P? evaluating the constant of integration which appears Pr, Prandtl number ; in the solution. 49 =2u,/v2 (K + 1)3; Q, total heat flux; BASIC ASSUMPTIONS Ra, = jlgL3(TL - T&q Rayleigh number; The height of the cavity is taken as H and the T, temperature; horizontal spacing of the walls as The vertical walls 11,w, velocity components, u = a*/az, w = L.
    [Show full text]
  • Summary of Dimensionless Numbers of Fluid Mechanics and Heat Transfer 1. Nusselt Number Average Nusselt Number: Nul = Convective
    Jingwei Zhu http://jingweizhu.weebly.com/course-note.html Summary of Dimensionless Numbers of Fluid Mechanics and Heat Transfer 1. Nusselt number Average Nusselt number: convective heat transfer ℎ퐿 Nu = = L conductive heat transfer 푘 where L is the characteristic length, k is the thermal conductivity of the fluid, h is the convective heat transfer coefficient of the fluid. Selection of the characteristic length should be in the direction of growth (or thickness) of the boundary layer; some examples of characteristic length are: the outer diameter of a cylinder in (external) cross flow (perpendicular to the cylinder axis), the length of a vertical plate undergoing natural convection, or the diameter of a sphere. For complex shapes, the length may be defined as the volume of the fluid body divided by the surface area. The thermal conductivity of the fluid is typically (but not always) evaluated at the film temperature, which for engineering purposes may be calculated as the mean-average of the bulk fluid temperature T∞ and wall surface temperature Tw. Local Nusselt number: hxx Nu = x k The length x is defined to be the distance from the surface boundary to the local point of interest. 2. Prandtl number The Prandtl number Pr is a dimensionless number, named after the German physicist Ludwig Prandtl, defined as the ratio of momentum diffusivity (kinematic viscosity) to thermal diffusivity. That is, the Prandtl number is given as: viscous diffusion rate ν Cpμ Pr = = = thermal diffusion rate α k where: ν: kinematic viscosity, ν = μ/ρ, (SI units : m²/s) k α: thermal diffusivity, α = , (SI units : m²/s) ρCp μ: dynamic viscosity, (SI units : Pa ∗ s = N ∗ s/m²) W k: thermal conductivity, (SI units : ) m∗K J C : specific heat, (SI units : ) p kg∗K ρ: density, (SI units : kg/m³).
    [Show full text]
  • Arxiv:1903.08882V2 [Physics.Flu-Dyn] 6 Jun 2019
    Lattice Boltzmann simulations of three-dimensional thermal convective flows at high Rayleigh number Ao Xua,∗, Le Shib, Heng-Dong Xia aSchool of Aeronautics, Northwestern Polytechnical University, Xi'an 710072, China bState Key Laboratory of Electrical Insulation and Power Equipment, Center of Nanomaterials for Renewable Energy, School of Electrical Engineering, Xi'an Jiaotong University, Xi'an 710049, China Abstract We present numerical simulations of three-dimensional thermal convective flows in a cubic cell at high Rayleigh number using thermal lattice Boltzmann (LB) method. The thermal LB model is based on double distribution function ap- proach, which consists of a D3Q19 model for the Navier-Stokes equations to simulate fluid flows and a D3Q7 model for the convection-diffusion equation to simulate heat transfer. Relaxation parameters are adjusted to achieve the isotropy of the fourth-order error term in the thermal LB model. Two types of thermal convective flows are considered: one is laminar thermal convection in side-heated convection cell, which is heated from one vertical side and cooled from the other vertical side; while the other is turbulent thermal convection in Rayleigh-B´enardconvection cell, which is heated from the bottom and cooled from the top. In side-heated convection cell, steady results of hydrodynamic quantities and Nusselt numbers are presented at Rayleigh numbers of 106 and 107, and Prandtl number of 0.71, where the mesh sizes are up to 2573; in Rayleigh-B´enardconvection cell, statistical averaged results of Reynolds and Nusselt numbers, as well as kinetic and thermal energy dissipation rates are presented at Rayleigh numbers of 106, 3×106, and 107, and Prandtl numbers of arXiv:1903.08882v2 [physics.flu-dyn] 6 Jun 2019 ∗Corresponding author Email address: [email protected] (Ao Xu) DOI: 10.1016/j.ijheatmasstransfer.2019.06.002 c 2019.
    [Show full text]
  • Thermodynamic and Transport Properties of Air and the Combustion Products of Natural Gas and of Astm-A-1 Fuel with Air
    NASA TECHNICAL NOTE -_.-NASA TN D-5 d. / d z c 4 w 4 z LOAN COPY: RETURN TO AFWL [WU-2) KIRTLAND AFB, N MEX THERMODYNAMIC AND TRANSPORT PROPERTIES OF AIR AND THE COMBUSTION PRODUCTS OF NATURAL GAS AND OF ASTM-A-1 FUEL WITH AIR by David J. Poferl, Roger A. Suehla, and Kenneth Lewandowski Lewis Research Center Cleveland, Ohio NATIONAL AERONAUTICS AND SPACE ADMINISTRATION WASHINGTON, D. C. OCTOBER 1969 d TECH LIBRARY KAFB, NM I 111111 11111 lllll1IIIII 1111 11111 Ill1 Ill 0053124 1. Report No. 2. Government Accession No. 3. Recipient's Lotolog No. NASA TN D - 54 52 Title and Subtitle I 5. Report Date 4. THERMODYNAMIC AND TRANSPORT PROPERTIES October 1969 OF AIR AND THE COMBUSTION PRODUCTS OF 6. Performing organization Code NATURAL GAS AND OF ASTM-A-1 FUEL WITH AIR 7. Authods) David J. Poferl, Roger A. Svehla, and 8. Performing Organization Report i Kenneth Lewandowski E-5122 9. Performing Organization Name and Address IO. Work Unit No. Lewis Research Center 720-03 11. Contract or Grant No. National Aeronautics and Space Administration Cleveland, Ohio 44135 13. Type of Report and Period Cov 12. Sponsoring Agency Name and Address Technical Note National Aeronautics and Space Administration Washington, D. C. 20546 14. Sponsoring Agency Code 15. Supplementary Notes 16. Abstract The ratio of specific heats, molecular weight, viscosity, specific heat at constant pr sure, thermal conductivity, and Prandtl number were calculated for air, the combus products of natural gas and air, and the combustion products of ASTM-A-1 jet fuel a air.
    [Show full text]
  • Thermophysical Properties of Helium-4 from 2 to 1500 K with Pressures to 1000 Atmospheres
    DATE DUE llbriZl<L. - ' :_ Demco, Inc. 38-293 National Bureau of Standards A UNITED STATES H1 DEPARTMENT OF v+ *^r COMMERCE NBS TECHNICAL NOTE 631 National Bureau of Standards PUBLICATION APR 2 1973 Library, E-Ol Admin. Bldg. OCT 6 1981 191103 Thermophysical Properties of Helium-4 from 2 to 1500 K with Pressures qc to 1000 Atmospheres joo U57Q lV-O/ U.S. >EPARTMENT OF COMMERCE National Bureau of Standards NATIONAL BUREAU OF STANDARDS 1 The National Bureau of Standards was established by an act of Congress March 3, 1901. The Bureau's overall goal is to strengthen and advance the Nation's science and technology and facilitate their effective application for public benefit. To this end, the Bureau conducts research and provides: (1) a basis for the Nation's physical measure- ment system, (2) scientific and technological services for industry and government, (3) a technical basis for equity in trade, and (4) technical services to promote public safety. The Bureau consists of the Institute for Basic Standards, the Institute for Materials Research, the Institute for Applied Technology, the Center for Computer Sciences and Technology, and the Office for Information Programs. THE INSTITUTE FOR BASIC STANDARDS provides the central basis within the United States of a complete and consistent system of physical measurement; coordinates that system with measurement systems of other nations; and furnishes essential services leading to accurate and uniform physical measurements throughout the Nation's scien- tific community, industry, and commerce. The Institute consists of a Center for Radia- tion Research, an Office of Measurement Services and the following divisions: Applied Mathematics—Electricity—Heat—Mechanics—Optical Physics—Linac Radiation 2—Nuclear Radiation 2—Applied Radiation 2 —Quantum Electronics3— Electromagnetics 3—Time and Frequency 3 —Laboratory Astrophysics 3—Cryo- 3 genics .
    [Show full text]