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Equilibrium Thermodynamic Properties Of Air Behind Incident Normal Shock Waves
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Book Synopsis Equilibrium Thermodynamic Properties of Air Behind Incident Normal Shock Waves by : Harry J. Davis
Download or read book Equilibrium Thermodynamic Properties of Air Behind Incident Normal Shock Waves written by Harry J. Davis and published by . This book was released on 1965 with total page 41 pages. Available in PDF, EPUB and Kindle. Book excerpt: The equilibrium temperature, density, and pressure of air behind incident normal shock waves have been calculated. The resulting tables include the effects of chemical reactions, excitation, dissociation, ionization, van der Waal and Coulomb forces. The tables are presented as functions of the ratio of the density behind the shock wave to the density at standard conditions in steps of 0.2. The temperature behind the shock wave T2 is a parameter which ranges from 2000K to 16,000K in 1000K steps. Two sets of tables, for initial conditions of 273.15 and 300.0K, are presented. The densities of air, as a real and as an ideal gas, are compared. (Author).
Book Synopsis Charts for Equilibrium Isentropic Expansion of Air Behind Shocks Up to 50,000 Per Second (15.24 Kilometers Per Second) by : Ernest V. Zoby
Download or read book Charts for Equilibrium Isentropic Expansion of Air Behind Shocks Up to 50,000 Per Second (15.24 Kilometers Per Second) written by Ernest V. Zoby and published by . This book was released on 1967 with total page 58 pages. Available in PDF, EPUB and Kindle. Book excerpt:
Book Synopsis Charts of Normal Shock Wave Properties in Imperfect Air by : Clark H. Lewis
Download or read book Charts of Normal Shock Wave Properties in Imperfect Air written by Clark H. Lewis and published by . This book was released on 1964 with total page 54 pages. Available in PDF, EPUB and Kindle. Book excerpt: Gas-dynamic properties which include the effects of dissociation, ionization, and intermolecular forces (van der Walls) are presented for incident and reflected shock waves in equilibrium imperfect air. Charts are presented for incident shock Mach numbers in the range from 6 to 30 into (ideal) air at a temperature of 300 K and pressures in the range from 10 to the minus 4 power to 10 to the 3rd power cm Hg. The temperature and density in any region do not exceed, respectively, 15,000 K and 158 amagats. In addition to the usual incident and reflected shock properties, stagnation conditions upstream and downstream and conditions immediately downstream of a standing shock wave are also presented. At pressures above one atmosphere in the undisturbed gas, the effects of the intermolecular forces on the gas-dynamic properties are demonstrated. (Author).
Book Synopsis Equilibrium Normal Shock Properties for Vibrationally Excited CO2-N2-He Gas Mixtures by : Michael T. Madden
Download or read book Equilibrium Normal Shock Properties for Vibrationally Excited CO2-N2-He Gas Mixtures written by Michael T. Madden and published by . This book was released on 1970 with total page 102 pages. Available in PDF, EPUB and Kindle. Book excerpt: Results are given for equilibrium properties behind incident and reflected normal shock waves in CO2-N2-He mixtures wherein the gas may be vibrationally excited but not chemically reacting. A rapid numerical iterative analysis is described, and the results are given in simple graphical form for convenient use in shock tube and shock tunnel experiments. The results are anticipated to be of particular use in determining reservoir conditions for shock tunnel experiments dealing with vibrational population inversions in rapidly expanding mixtures. (Author).
Book Synopsis Normal Shock Wave Parameters in Equilibrium Air by : Charles E. Wittliff
Download or read book Normal Shock Wave Parameters in Equilibrium Air written by Charles E. Wittliff and published by . This book was released on 1961 with total page 102 pages. Available in PDF, EPUB and Kindle. Book excerpt: Tables and graphs are given of normal shock wave parameters for equilibrium air. Composition of the air behind the shock is also tabulated. The results cover the range of velocities from 2000 to 26,000 fps in increments of 1000 fps and altitudes from sea level to 300,000 ft at 10,000ft intervals. The 1959 ARDC model atmosphere was used to specify ambient conditions ahead of the shock. An effective specific heat ratio, was tabulated which permits solution of oblique shock waves.
Book Synopsis Thermodynamic Properties of Carbon-dioxide and Nitrogen Mixtures Behind a Normal Shock Wave by : Henry T. Woodward
Download or read book Thermodynamic Properties of Carbon-dioxide and Nitrogen Mixtures Behind a Normal Shock Wave written by Henry T. Woodward and published by . This book was released on 1963 with total page 40 pages. Available in PDF, EPUB and Kindle. Book excerpt:
Book Synopsis Equilibrium Properties of Air Behind Normal Shock Waves by : Harry John Davis
Download or read book Equilibrium Properties of Air Behind Normal Shock Waves written by Harry John Davis and published by . This book was released on 1964 with total page 92 pages. Available in PDF, EPUB and Kindle. Book excerpt:
Book Synopsis A Graphical Solution of Shock Equations by : Charles E. Treanor
Download or read book A Graphical Solution of Shock Equations written by Charles E. Treanor and published by . This book was released on 1959 with total page 88 pages. Available in PDF, EPUB and Kindle. Book excerpt:
Book Synopsis Normal Shock Waves in Air: Equilibrium Composition and Flow Parameters for Velocities from 26,000 to 50,000 Ft/sec by : Paul V. Marrone
Download or read book Normal Shock Waves in Air: Equilibrium Composition and Flow Parameters for Velocities from 26,000 to 50,000 Ft/sec written by Paul V. Marrone and published by . This book was released on 1962 with total page 98 pages. Available in PDF, EPUB and Kindle. Book excerpt:
Book Synopsis High Temperature Phenomena in Shock Waves by : Raymond Brun
Download or read book High Temperature Phenomena in Shock Waves written by Raymond Brun and published by Springer Science & Business Media. This book was released on 2012-01-24 with total page 344 pages. Available in PDF, EPUB and Kindle. Book excerpt: The high temperatures generated in gases by shock waves give rise to physical and chemical phenomena such as molecular vibrational excitation, dissociation, ionization, chemical reactions and inherently related radiation. In continuum regime, these processes start from the wave front, so that generally the gaseous media behind shock waves may be in a thermodynamic and chemical non-equilibrium state. This book presents the state of knowledge of these phenomena. Thus, the thermodynamic properties of high temperature gases, including the plasma state are described, as well as the kinetics of the various chemical phenomena cited above. Numerous results of measurement and computation of vibrational relaxation times, dissociation and reaction rate constants are given, and various ionization and radiative mechanisms and processes are presented. The coupling between these different phenomena is taken into account as well as their interaction with the flow-field. Particular points such as the case of rarefied flows and the inside of the shock wave itself are also examined. Examples of specific non-equilibrium flows are given, generally corresponding to those encountered during spatial missions or in shock tube experiments.
Book Synopsis Scientific and Technical Aerospace Reports by :
Download or read book Scientific and Technical Aerospace Reports written by and published by . This book was released on 1977 with total page 276 pages. Available in PDF, EPUB and Kindle. Book excerpt:
Book Synopsis Tables of Normal Shock Wave Properties for Oxygen and Nitrogen in Dissociation Equilibrium by : C. K. Law
Download or read book Tables of Normal Shock Wave Properties for Oxygen and Nitrogen in Dissociation Equilibrium written by C. K. Law and published by . This book was released on 1969 with total page 16 pages. Available in PDF, EPUB and Kindle. Book excerpt: An accurate table for the gasdynamic properties behind incident and reflected normal shock waves was constructed for gaseous oxygen and nitrogen in dissociation equilibrium. The values of the temperature and pressure behind the respective shocks were computed to within 0.1% of the exact root. Second order correction factors for the molecular rotation function were also taken into account. The initial temperature is taken to be 298.13K for all cases, the initial pressures cover the range from 0.01 to 2000 mmHg and the incident shock Mach number is varied in increments of 0.1 from 6 to 18. The computer program was written in such a way that only slight modifications are needed for its use with other gases and other states of equilibrium. (Author).
Book Synopsis Physics of Shock Waves and High–Temperature Hydrodynamic Phenomena by : Wallace Hayes
Download or read book Physics of Shock Waves and High–Temperature Hydrodynamic Phenomena written by Wallace Hayes and published by Elsevier. This book was released on 2012-12-02 with total page 479 pages. Available in PDF, EPUB and Kindle. Book excerpt: Physics of Shock Waves and High-Temperature Hydrodynamic Phenomena, Volume II presents interpretations of the physical basis of shockwaves and high-temperature hydrodynamic phenomena and gives practical guidance to those who work with these subjects in science and modern technology. This volume contains chapters discussing such topics as the shockwave structure in gases; physical and chemical kinetics in hydrodynamic processes; the radiative phenomena in shock waves and in strong explosions in the air; thermal waves and shockwaves in solids; and self-similar processes in gasdynamics. Physicists, engineers, researchers, and professors and students in the field of the physical sciences will find the book very educational.
Book Synopsis Charts for Equilibrium and Frozen Flows Across Plane Shock Waves in Carbon Dioxide by : Craig D. Simcox
Download or read book Charts for Equilibrium and Frozen Flows Across Plane Shock Waves in Carbon Dioxide written by Craig D. Simcox and published by . This book was released on 1965 with total page 140 pages. Available in PDF, EPUB and Kindle. Book excerpt:
Download or read book Technical Abstract Bulletin written by and published by . This book was released on with total page 684 pages. Available in PDF, EPUB and Kindle. Book excerpt:
Download or read book NASA Technical Translation written by and published by . This book was released on 1969 with total page 1032 pages. Available in PDF, EPUB and Kindle. Book excerpt:
Book Synopsis Government Reports Announcements by :
Download or read book Government Reports Announcements written by and published by . This book was released on 1975-03 with total page 898 pages. Available in PDF, EPUB and Kindle. Book excerpt:
