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  • FLUID MECHANICS AND HEAT TRANSFER  (7)
  • (Bovine cardiac sarcolemma)  (1)
  • China  (1)
  • 1
    Electronic Resource
    Electronic Resource
    Kinetic characterization and radiation-target sizing of the glucose transporter in cardiac sarcolemmal vesicles
    Amsterdam : Elsevier
    Biochimica et Biophysica Acta (BBA)/Biomembranes 943 (1988), S. 360-366 
    Details
    ISSN: 0005-2736
    Keywords: (Bovine cardiac sarcolemma) ; Glucose transporter ; Kinetics ; Radiation-target sizing
    Source: Elsevier Journal Backfiles on ScienceDirect 1907 - 2002
    Topics: Biology , Chemistry and Pharmacology , Medicine , Physics
    Type of Medium: Electronic Resource
    URL: http://dx.doi.org/10.1016/0005-2736(88)90568-8
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    Paper (German National Licenses)
    Fulltext
  • 2
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    Active subduction and collision in Southeast Asia (2001)
    In:  Tectonophys., Basel, Elsevier Science Publishers, vol. 333, no. 1-2, pp. 1-7, pp. 2519, (ISSN: 1340-4202)
    Details
    Publication Date: 2001
    Keywords: Review article ; Plate tectonics ; China ; Taiwan ; Kamchatka ; Japan ; Philippines ; Indonesia ; Papua ; New ; Guinea
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    BIBLIOGRAPHY SEISMOLOGY
  • 3
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    Three-dimensional calculations of supersonic reacting flows using an LU scheme (1992)
    In:  Other Sources
    Details
    Publication Date: 2011-08-24
    Description: An implicit finite volume lower-upper time-marching method which efficiently solves the complete Navier-Stokes and specied equations in a fully coupled fashion is the basis of the present 3D numerical program for simulating the supersonic reacting flows of H2 in air. The chemistry model incorporated has nine species and 18 reaction steps. Calculations are presented for flowfields of underexpanded hydrogen jets that are transversely injected into the supersonic airstream within scramjet combustors; the shock structure, separated flow regions around the injector, and combustion-product distributions are clearly represented.
    Keywords: FLUID MECHANICS AND HEAT TRANSFER
    Type: Journal of Computational Physics (ISSN 0021-9991); 101; 2, Au
    Format: text
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    NASA TECHNICAL REPORTS
  • 4
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    Recent update of the RPLUS2D/3D codes (1991)
    In:  CASI
    Details
    Publication Date: 2019-06-28
    Description: The development of the RPLUS2D/3D codes is summarized. These codes utilize LU algorithms to solve chemical non-equilibrium flows in a body-fitted coordinate system. The motivation behind the development of these codes is the need to numerically predict chemical non-equilibrium flows for the National AeroSpace Plane Program. Recent improvements include vectorization method, blocking algorithms for geometric flexibility, out-of-core storage for large-size problems, and an LU-SW/UP combination for CPU-time efficiency and solution quality.
    Keywords: FLUID MECHANICS AND HEAT TRANSFER
    Type: NASA, Lewis Research Center, Computational Fluid Dynamics Symposium on Aeropropulsion; p 593-607
    Format: application/pdf
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    NASA TECHNICAL REPORTS
  • 5
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    Comparative study of computational efficiency of two LU schemes for non-equilibrium reacting flows (1990)
    In:  Other Sources
    Details
    Publication Date: 2019-06-28
    Description: The systems of equations governing chemically nonequilibrium flows are solved numerically by two lower-upper(LU) algorithms, namely, LU-SSOR (Yoon and Jameson, 1987) and LU-SW (Steger and Warming, 1981). The methods of flux-Jacobian splitting differentiate the two LU algorithms. The LU-SSOR gives a simpler implicit operator with less temporal damping, while the LU-SW converges faster but requires more computation for each iteration. Relative efficiencies and mutual merits of these two LU algorithms are compared. The results show that LU-SW with upwind-differenced right-hand-side gives the best convergence.
    Keywords: FLUID MECHANICS AND HEAT TRANSFER
    Type: AIAA PAPER 90-0396
    Format: text
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    NASA TECHNICAL REPORTS
  • 6
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    Runge-Kutta methods combined with compact difference schemes for the unsteady Euler equations (1992)
    In:  Other Sources
    Details
    Publication Date: 2019-06-28
    Description: An investigation of the Runge-Kutta time-stepping, combined with compact difference schemes to solve the unsteady Euler equations, is presented. Initially, a generalized form of a N-step Runge-Kutta technique is derived. By comparing this generalized form with its Taylor's series counterpart, the criteria for the three-step and four-step schemes to be of third- and fourth-order accurate are obtained.
    Keywords: FLUID MECHANICS AND HEAT TRANSFER
    Type: AIAA PAPER 92-3210
    Format: text
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    NASA TECHNICAL REPORTS
  • 7
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    Three-dimensional calculation of supersonic reacting flows using an LU scheme (1989)
    In:  Other Sources
    Details
    Publication Date: 2019-06-28
    Description: A new three-dimensional numerical program incorporated with comprehensive real gas property models has been developed to simulate supersonic reacting flows. The code employs an implicit finite volume, Lower-Upper (LU) time-marching method to solve the complete Navier-Stokes and species equations in a fully-coupled and very efficient manner. A chemistry model with nine species and eighteen reaction steps are adopted in the program to represent the chemical reaction of H2 and air. To demonstrate the capability of the program, flow fields of underexpanded hydrogen jets transversely injected into supersonic air stream inside the combustors of scramjets are calculated. Results clearly depict the flow characteristics, including the shock structure, separated flow regions around the injector, and the distribution of the combustion products.
    Keywords: FLUID MECHANICS AND HEAT TRANSFER
    Type: AIAA PAPER 89-0391
    Format: text
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    NASA TECHNICAL REPORTS
  • 8
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    Probability density function approach for compressible turbulent reacting flows (1994)
    In:  Other Sources
    Details
    Publication Date: 2019-07-13
    Description: The objective of the present work is to extend the probability density function (PDF) tubulence model to compressible reacting flows. The proability density function of the species mass fractions and enthalpy are obtained by solving a PDF evolution equation using a Monte Carlo scheme. The PDF solution procedure is coupled with a compression finite-volume flow solver which provides the velocity and pressure fields. A modeled PDF equation for compressible flows, capable of treating flows with shock waves and suitable to the present coupling scheme, is proposed and tested. Convergence of the combined finite-volume Monte Carlo solution procedure is discussed. Two super sonic diffusion flames are studied using the proposed PDF model and the results are compared with experimental data; marked improvements over solutions without PDF are observed.
    Keywords: FLUID MECHANICS AND HEAT TRANSFER
    Type: AIAA Journal (ISSN 0001-1452); 32; 7; p. 1407-1415
    Format: text
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  • 9
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    PDF approach for compressible turbulent reacting flows (1993)
    In:  Other Sources
    Details
    Publication Date: 2019-07-13
    Description: The objective of the present work is to develop a probability density function (pdf) turbulence model for compressible reacting flows for use with a CFD flow solver. The probability density function of the species mass fraction and enthalpy are obtained by solving a pdf evolution equation using a Monte Carlo scheme. The pdf solution procedure is coupled with a compressible CFD flow solver which provides the velocity and pressure fields. A modeled pdf equation for compressible flows, capable of capturing shock waves and suitable to the present coupling scheme, is proposed and tested. Convergence of the combined finite-volume Monte Carlo solution procedure is discussed, and an averaging procedure is developed to provide smooth Monte-Carlo solutions to ensure convergence. Two supersonic diffusion flames are studied using the proposed pdf model and the results are compared with experimental data; marked improvements over CFD solutions without pdf are observed. Preliminary applications of pdf to 3D flows are also reported.
    Keywords: FLUID MECHANICS AND HEAT TRANSFER
    Type: AIAA PAPER 93-0087 , AIAA, Aerospace Sciences Meeting and Exhibit; Jan 11, 1993 - Jan 14, 1993; Reno, NV; United States|; 16 p.
    Format: text
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    NASA TECHNICAL REPORTS
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