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Books on the topic 'Ideal gas flow'

Author: Grafiati

Published: 4 June 2021

Last updated: 29 July 2025

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1

Center, Ames Research, ed. Steady secondary flows generated by periodic compression and expansion of an ideal gas in a pulse tube. National Aeronautics and Space Administration, Ames Research Center, 1999.

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2

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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3

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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4

R, Edwards Jack, and NASA Glenn Research Center, eds. Numerical speed of sound and its application to schemes for all speeds. National Aeronautics and Space Administration, Glenn Research Center, 1999.

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5

R, Edwards Jack, and NASA Glenn Research Center, eds. Numerical speed of sound and its application to schemes for all speeds. National Aeronautics and Space Administration, Glenn Research Center, 1999.

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6

R, Millman Daniel, Greendyke Robert B, and United States. National Aeronautics and Space Administration. Scientific and Technical Information Program., eds. Finite-differnce solution for laminar or turbulent boundary layer flow over axisymmetric bodies with ideal gas, CF, or equilibrium air chemistry. National Aeronautics and Space Administration, Office of Management, Scientific and Technical Information Program, 1992.

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7

R, Millman Daniel, Greendyke Robert B, and United States. National Aeronautics and Space Administration. Scientific and Technical Information Program., eds. Finite-difference solution for laminar or turbulent boundary layer flow over axisymmetric bodies with ideal gas, CF,́ or equilibrium air chemistry. National Aeronautics and Space Administration, Office of Management, Scientific and Technical Information Program, 1992.

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8

R, Millman Daniel, Greendyke Robert B, and United States. National Aeronautics and Space Administration. Scientific and Technical Information Program., eds. Finite-differnce solution for laminar or turbulent boundary layer flow over axisymmetric bodies with ideal gas, CF, or equilibrium air chemistry. National Aeronautics and Space Administration, Office of Management, Scientific and Technical Information Program, 1992.

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9

W, Paulson John, Weilmuenster K. James, and United States. National Aeronautics and Space Administration., eds. Experimental and computational analysis of shuttle orbiter hypersonic trim anomaly. American Institute of Aeronautics and Astronautics, 1995.

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10

R, Spall John, and Langley Research Center, eds. Time-dependent solution for axisymmetric flow over a blunt body with ideal gas, CF,□ or equilibrium air chemistry. National Aeronautics and Space Administration, Langley Research Center, 1987.

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11

R, Spall John, and Langley Research Center, eds. Time-dependent solution for axisymmetric flow over a blunt body with ideal gas, CF, or equilibrium air chemistry. National Aeronautics and Space Administration, Langley Research Center, 1987.

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12

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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13

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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14

Hamilton, H. Harris. Finite-difference solution for laminar or turbulent boundary layer flow over axisymmetric bodies with ideal gas, CF4, or equilibrium air chemistry. Langley Research Center, 1992.

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15

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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16

Tatum, Kenneth E. Computation of thermally perfect properties of oblique shock waves. Institute for Computer Applications in Science and Engineering, NASA Langley Research Center, 1996.

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17

Center, Langley Research, ed. Computation of thermally perfect properties of oblique shock waves: Under contract NAS1-19000. National Aeronautics and Space Administration, Langley Research Center, 1996.

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18

Center, Langley Research, ed. Computation of thermally perfect properties of oblique shock waves: Under contract NAS1-19000. National Aeronautics and Space Administration, Langley Research Center, 1996.

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19

Ciappei, Cristiano, ed. Innovazione e brokeraggio tecnologico. Firenze University Press, 2010. http://dx.doi.org/10.36253/978-88-8453-983-0.

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This book is designed to furnish Italian literature with an insight into the significance and the role of knowledge transfer, and in particular of technological brokerage. The idea is that, in the present-day world, dominated by a technology and knowledge available to an increasingly large number of people, enterprises are called upon to reconfigure the concept of innovation, expanding in even geographical terms the quest for solutions that aim at creating an exchange of interdisciplinary knowledge. To respond to the need for the dissemination of knowledge, collaboration between enterprises an

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20

On the Görtler instability in hypersonic flows: Sutherland law fluids and real gas effects. National Aeronautics and Space Administration, Langley Research Center, Institute for Computer Applications in Science and Engineering, 1990.

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21

On the Görtler instability in hypersonic flows: Sutherland law fluids and real gas effects. National Aeronautics and Space Administration, Langley Research Center, Institute for Computer Applications in Science and Engineering, 1990.

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22

Experimental and computational analysis of shuttle orbiter hypersonic trim anomaly. American Institute of Aeronautics and Astronautics, 1995.

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23

Time-dependent solution for axisymmetric flow over a blunt body with ideal gas, CF, or equilibrium air chemistry. National Aeronautics and Space Administration, Langley Research Center, 1987.

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24

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

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25

Sherwood, Dennis, and Paul Dalby. Temperature and heat. Oxford University Press, 2018. http://dx.doi.org/10.1093/oso/9780198782957.003.0003.

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Concepts of temperature, temperature scales and temperature measurement. The ideal gas law, Dalton’s law of partial pressure. Assumptions underlying the ideal gas, and distinction between ideal and real gases. Introduction to equations-of-state such as the van der Waals, Dieterici, Berthelot and virial equations, which describe real gases. Concept of heat, and distinction between heat and temperature. Experiments of Rumford and Joule, and the principle of the conservation of energy. Units of measurement for heat. Heat as a path function. Flow of heat down a temperature gradient as an irreversi

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26

Clarke, Andrew. Energy and heat. Oxford University Press, 2017. http://dx.doi.org/10.1093/oso/9780199551668.003.0002.

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Energy is the capacity to do work and heat is the spontaneous flow of energy from one body or system to another through the random movement of atoms or molecules. The entropy of a system determines how much of its internal energy is unavailable for work under isothermal conditions, and the Gibbs energy is the energy available for work under isothermal conditions and constant pressure. The Second Law of Thermodynamics states that for any reaction to proceed spontaneously the total entropy (system plus surroundings) must increase, which is why metabolic processes release heat. All organisms are

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27

Hendrickx, Jan F. A., André van Zundert, and Andre De Wolf. Inhaled anaesthetics. Edited by Michel M. R. F. Struys. Oxford University Press, 2017. http://dx.doi.org/10.1093/med/9780199642045.003.0014.

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Inhaled anaesthetic drugs are administered via the lungs to provide ‘general anaesthesia’. They are considered complete anaesthetics because they in and by themselves can in most patients ensure all clinical end-points that are required for ‘general anaesthesia’ (unconsciousness, immobility, and haemodynamic stability). The dose–response curve of each clinical end-point is conveniently defined by its mid-point, the end-expired concentration Fa that ensures response suppression in 50 % of the patients (MACawake, MAC, and MACBAR). By understanding the dose–response curves and the factors that in

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28

Wolf, E. L. Physics and Technology of Sustainable Energy. Oxford University Press, 2018. http://dx.doi.org/10.1093/oso/9780198769804.001.0001.

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This is a physics textbook describing, at a college level, the physics and technology needed to provide sustainable long-term energy, past the era of fossil fuels. A summary is given of global power generation and consumption, with estimates of times until conventional fuels will deplete. Sustainable power sources, largely those coming from the Sun directly or indirectly, are described. As sustainable energy must preserve the Earth’s atmosphere and climate, key elements of these topics are included. Key energy technologies in this book include photovoltaics, wind turbines and the electric powe

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