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Books on the topic 'Gaz compressibles'

Author: Grafiati

Published: 4 June 2021

Last updated: 3 February 2022

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1

Yahya, S. M. Gas tables for compressible flow calculations. 5th ed. New Age International (P) Ltd., Publishers, 2006.

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2

Modern compressible flow: With historical perspective. 3rd ed. McGraw-Hill, 2003.

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3

Modern compressible flow: With historical perspective. 2nd ed. McGraw-Hill, 1990.

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4

Délery, J. Handbook of compressible aerodynamics. ISTE, 2010.

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5

Handbook of compressible aerodynamics. ISTE, 2010.

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6

Wang, B. Y. Compressible laminar boundary-layer flows of a dusty gas over a semi-infinite flat plate. [s.n.], 1988.

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7

Husain, Zoeb. Compressible flow through problems or gas dynamics through problems. Wiley, 1989.

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8

Perthame, B. On positively preserving finite volume schemes for compressible Euler Equations. National Aeronautics and Space Administration, Langley Research Center, 1993.

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9

Perthame, Benoit. On positively preserving finite volume schemes for compressible Euler Equations. National Aeronautics and Space Administration, Langley Research Center, 1993.

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10

Roe, P. L. Remote boundary conditions for unsteady multidimensional aerodynamic computations. National Aeronautics and Space Administration, Langley Research Center, 1987.

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11

Roe, P. L. Remote boundary conditions for unsteady multidimensional aerodynamic computations. ICASE, 1986.

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12

Xu, Kun. A gas-kinetic BGK scheme for the compressible Navier-Stokes equations. National Aeronautics and Space Administration, Langley Research Center, 2000.

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13

Wong, C. Channy. A domain decomposition study of massively parallel computing in compressible gas dynamics. American Institute of Aeronautics and Astronautics, 1995.

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14

Gnoffo, Peter A. An upwind-biased, point-implicit relaxation algorithm for viscous, compressible perfect-gas flows. National Aeronautics and Space Administration, Office of Management, Scientific and Technical Information Division, 1990.

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15

Gnoffo, Peter A. An upwind-biased, point-implicit relaxation algorithm for viscous, compressible perfect-gas flows. Langley Research Center, 1990.

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16

Gnoffo, Peter A. An upwind-biased, point-implicit relaxation algorithm for viscous, compressible perfect-gas flows. National Aeronautics and Space Administration, Office of Management, Scientific and Technical Information Division, 1990.

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17

Chisum, James E. Simulation of the dynamic behavior of explosion gas bubbles in a compressible fluid medium. Naval Postgraduate School, 1996.

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18

Lui, Shiu-Hong. Entropy analysis of kinetic flux vector splitting schemes for the compressible Euler equations. Institute for Computer Applications in Science and Engineering, NASA Langley Research Center, 1999.

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19

Witte, David W. Computer code for determination of thermally perfect gas properties. National Aeronautics and Space Administration, Langley Research Center, 1994.

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20

Wang, B. Y. Asymptotic solutions to compressible laminar boundary-layer solutions for dusty-gas flow over a semi-infinite flat plate. Institute for Aerospace Studies, 1986.

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21

Wang, B. Y. Finite-difference solutions for compressible laminar boundary-layer flows of a dusty gas over a semi-infinite flat plate. Institute for Aerospace Studies, 1986.

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22

Keenan, Joseph Henry. Gas tables: Thermodynamic properties of air products of combustion and component gases, compressible flow functions : including those of Ascher H. Shapiro and Gilbert M. Edelman. 2nd ed. Krieger Pub. Co., 1992.

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23

Keenan, Joseph Henry. Gas tables: International version : thermodynamic properties of air products of combustion and component gases compressible flow functions, including those of Ascher H. Shapiro and Gilbert M. Edelman. 2nd ed. Krieger Pub. Co., 1992.

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24

Anderson, John. Modern Compressible Flow. OPEN UNIVERSITY PRES, 2004.

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25

Anderson, John. Modern Compressible Flow. OPEN UNIVERSITY PRES, 2004.

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26

Escudier, Marcel. Compressible pipe flow. Oxford University Press, 2018. http://dx.doi.org/10.1093/oso/9780198719878.003.0013.

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In this chapter gas flow through pipes is analysed, taking account of compressibility and either friction or heat exchange with the fluid. It is shown that in all cases the key parameter is the Mach number. The analyses are based upon the conservation laws for mass, momentum, and energy, together with an equation of state. So that significant results can be achieved, the flowing fluid is treated as a perfect gas, and the flow as one dimensional. Adiabatic pipe flow with wall friction is termed Fanno flow. Frictionless pipe flow with heat transfer is termed Rayleigh flow. It is found that both

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27

Escudier, Marcel. Compressible fluid flow. Oxford University Press, 2018. http://dx.doi.org/10.1093/oso/9780198719878.003.0011.

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Compressible-gas flow through convergent and convergent-divergent nozzles is analysed in this chapter based upon the conservation laws for mass, momentum, and energy, together with considerations of thermodynamics. It is shown that in both cases the key parameter in describing the flow is the Mach number, which is used to distinguish between subsonic and supersonic flow. So that significant results can be achieved, the flowing fluid is treated as a perfect gas, and the flow as one dimensional. Flow through a convergent nozzle and the choking limitation is discussed. Flow through a normal shock

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28

Wiley. Gas Tables for Compressible Flow Calculations. John Wiley & Sons, 1986.

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29

Anderson, John, and John D. Anderson. Modern Compressible Flow: With Historical Perspective. 3rd ed. McGraw-Hill Science/Engineering/Math, 2002.

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30

Anderson, John, and John D. Anderson. Modern Compressible Flow: With Historical Perspective. McGraw-Hill Science/Engineering/Math, 2002.

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31

Jr, Anderson John D. Modern Compressible Flow: With Historical Perspective. McGraw-Hill Higher Education, 2020.

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32

Jr, Anderson John D. Modern Compressible Flow: With Historical Perspective. McGraw-Hill Higher Education, 2020.

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33

K, Johnson D., and United States. National Aeronautics and Space Administration., eds. Boundary conditions for unsteady compressible flows. National Aeronautics and Space Administration, 1994.

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34

E, Hurlburt Neal, Toomre J. 1940-, and United States. National Aeronautics and Space Administration., eds. Turbulent compressible convection with rotation. National Aeronautics and Space Administration, 1998.

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35

Turbulent compressible convection with rotation. National Aeronautics and Space Administration, 1996.

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36

The stability of compressible mixing layers in binary cases. Institute for Computer Applications in Science and Engineering, NASA Langley Research Center, 1996.

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37

Modern Compressible Flow: With Historical Perspective (Mcgraw-Hill Series in Aeronautical and Aerospace Engineering). 3rd ed. McGraw-Hill Companies, 2002.

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38

The structure of variable property, compressible mixing layers in binary gas mixtures. Institute for Computer Applications in Science and Engineering, NASA Langley Research Center, 1996.

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39

Simulation of the Dynamic Behavior of Explosion Gas Bubbles in a Compressible Fluid Medium. Storming Media, 1996.

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40

E, Tatum Kenneth, and Langley Research Center, eds. Computer code for determination of thermally perfect gas properties. National Aeronautics and Space Administration, Langley Research Center, 1994.

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41

Institute for Computer Applications in Science and Engineering., ed. Some developments of the equilibrium particle simulation method for the direct simulation of compressible flows. Institute for Computer Applications in Science and Engineering, NASA Langley Research Center, 1995.

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42

Kun, Xu, and Institute for Computer Applications in Science and Engineering., eds. A gas-kinetic scheme for reactive flows. Institute for Computer Applications in Science and Engineering, NASA Langley Research Center, 1998.

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43

Kun, Xu, and Institute for Computer Applications in Science and Engineering., eds. A gas-kinetic scheme for reactive flows. Institute for Computer Applications in Science and Engineering, NASA Langley Research Center, 1998.

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44

Kun, Xu, and Institute for Computer Applications in Science and Engineering., eds. A gas-kinetic scheme for reactive flows. Institute for Computer Applications in Science and Engineering, NASA Langley Research Center, 1998.

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45

Kun, Xu, and Institute for Computer Applications in Science and Engineering., eds. A gas-kinetic scheme for reactive flows. Institute for Computer Applications in Science and Engineering, NASA Langley Research Center, 1998.

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46

Escudier, Marcel. Introduction to Engineering Fluid Mechanics. Oxford University Press, 2018. http://dx.doi.org/10.1093/oso/9780198719878.001.0001.

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Turbojet and turbofan engines, rocket motors, road vehicles, aircraft, pumps, compressors, and turbines are examples of machines which require a knowledge of fluid mechanics for their design. The aim of this undergraduate-level textbook is to introduce the physical concepts and conservation laws which underlie the subject of fluid mechanics and show how they can be applied to practical engineering problems. The first ten chapters are concerned with fluid properties, dimensional analysis, the pressure variation in a fluid at rest (hydrostatics) and the associated forces on submerged surfaces, t

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47

Somasundaram, Pr S. L. Gas Dynamics and Jet Propulsion ; Comprehensive Book in S.L. Units, More than 50 Solved Problems, Additional 150 Problems with Answer, Properties of Air and Compressible Flow function Table. New Age International (P) Ltd., 1996.

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48

N, Tiwari S., and United States. National Aeronautics and Space Administration., eds. Numerical solutions of Navier-Stokes equations for a Butler wing. Old Dominion University Research Foundation, 1987.

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49

N, Tiwari S., and Langley Research Center, eds. Numerical solutions of Navier-Stokes equations for a Butler wing: Progress report for the period ending August 31, 1985. Old Dominion University Research Foundation, 1985.

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