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Charts Of Normal Shock Wave Properties In Imperfect Air
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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 Charts of Normal Shock Wave Properties in Imperfect Air (supplement: MS by : Clark H. Lewis
Download or read book Charts of Normal Shock Wave Properties in Imperfect Air (supplement: MS written by Clark H. Lewis and published by . This book was released on 1965 with total page 57 pages. Available in PDF, EPUB and Kindle. Book excerpt:
Book Synopsis Charts of Normal Shock Wave Properties in Imperfect Nitrogen (supplement: M Sub S by : Clark H. LEWIS
Download or read book Charts of Normal Shock Wave Properties in Imperfect Nitrogen (supplement: M Sub S written by Clark H. LEWIS and published by . This book was released on 1966 with total page 58 pages. Available in PDF, EPUB and Kindle. Book excerpt: Gas dynamic properties which include the effects of dissociation and intermolecular forces (van der Waals) are presented for incident and reflected shock waves in equilibrium imperfect nitrogen. Charts are presented for incident shock Mach numbers in the range from 1 to 10 into (ideal) nitrogen at a temperature of 300K and pressures in the range from 0.0001 to 1000 cm Hg. The temperature and density in any region do not exceed, respectively, 15,000K and 1000 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 Charts of Normal Shock Wave Properties in Imperfect Nitrogen by : Clark H. Lewis
Download or read book Charts of Normal Shock Wave Properties in Imperfect Nitrogen 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 nitrogen. Charts are presented for incident shock Mach numbers in the range from 4 to 30 into (ideal) nitrogen at a temperature of 300 K and pressures in the range from 0.0010 to 10000 cm Hg. The temperature and density in any region do not exceed, respectively, 15,000 K and 150 amagats. In addi tion 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 gasdynamic properties are demonstrated. (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 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 Altitude-velocity Table and Charts for Imperfect Air by : Clark Houston Lewis
Download or read book Altitude-velocity Table and Charts for Imperfect Air written by Clark Houston Lewis and published by . This book was released on 1965 with total page 70 pages. Available in PDF, EPUB and Kindle. Book excerpt:
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 Shock Tubes by : Irving Israel Glass
Download or read book Shock Tubes written by Irving Israel Glass and published by University of Toronto Press. This book was released on 1970-12-15 with total page 852 pages. Available in PDF, EPUB and Kindle. Book excerpt: This volume contains the proceedings of a symposium held at the University of Toronto in June 1969. The symposium consisted of six sessions; each containing an invited paper, followed by six contributed papers reporting on recent, relevant research and development. The topics are: a review of research problems in basic shock tube flows and the possibilities for the shock tube in the future; driving techniques; explosive drivers; theoretical and experimental research in electromagnetic shock tubes; chemical kinetics and spectroscopy; and a review of shock tube diagnostics, instrumentation and fundamental data as well as the measurement of physical quantities.
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 1994 with total page 892 pages. Available in PDF, EPUB and Kindle. Book excerpt:
Book Synopsis Study of High-density Hypervelocity Flows and Similitudes by : Cornell Aeronautical Laboratory
Download or read book Study of High-density Hypervelocity Flows and Similitudes written by Cornell Aeronautical Laboratory and published by . This book was released on 1967 with total page 320 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 U.S. Government Research Reports by :
Download or read book U.S. Government Research Reports written by and published by . This book was released on 1964 with total page 250 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 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:
Download or read book NASA Technical Note written by and published by . This book was released on 1967 with total page 594 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:
