Charts for Equilibrium Isentropic Expansion of Air Behind Shocks Up to 50,000 Per Second (15.24 Kilometers Per Second) PDF Download
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Author: Ernest V. Zoby
Publisher:
ISBN:
Category : Air
Languages : en
Pages : 58
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Book Description
Author: Ernest V. Zoby
Publisher:
ISBN:
Category : Air
Languages : en
Pages : 58
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Book Description
Author: Ernest V. Zoby
Publisher:
ISBN:
Category : Air
Languages : en
Pages : 0
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Book Description
Author: Ernest V. Zoby
Publisher:
ISBN:
Category : Aerodynamics
Languages : en
Pages : 49
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Book Description
Author: William L. Grose
Publisher:
ISBN:
Category : Air
Languages : en
Pages : 32
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Book Description
Charts are presented which facilitate the theoretical analysis of certain flow processes involving an unsteady expansion wave in equilibrium real air. The parameters evaluated are related to (a) the velocity change in an unsteady expansion wave, (b) the maximum velocity attainable in a shock-wave--expansion-wave cycle, (c) the time for characteristic traversal through an expansion wave, and (d) the entropy in shock-initiated flows. Such parameters are of particular interest in analysis of the shock-initiated expansion-tube cycle.
Author: Paul V. Marrone
Publisher:
ISBN:
Category : Shock waves
Languages : en
Pages : 98
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Book Description
Author: Charles George Miller
Publisher:
ISBN:
Category : Aerothermodynamics
Languages : en
Pages : 298
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Book Description
Properties include pressure, temperature, density, enthalpy, speed of sound, entropy, molecular weight ratio, isentropic exponent, velocity, and species mole fractions. Incident (moving) shock velocities are varied from 1 to 16 km/sec for a range of initial pressure of 5 N/sq m to 500 kN/sq m. Working charts illustrating idealized shock tube performance with CO2 test gas and heated helium and hydrogen driver gases are also presented.
Author: Richard W. Ziemer
Publisher:
ISBN:
Category : Aerodynamics, Hypersonic
Languages : en
Pages : 86
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Book Description
Author: Charles George Miller
Publisher:
ISBN:
Category : Aerothermodynamics
Languages : en
Pages : 324
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Book Description
Author: Charles A. Cook
Publisher:
ISBN:
Category : Shock waves
Languages : en
Pages : 48
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Book Description
New calculations of the equilibrium gas proper ties behind a normal shock wave are presented based on the 1959 ARDC Model Atmosphere. Graphs of pressure, density, and temperat8re are pre sented for conditions behind a normal shock wave and at the stagnation point following an isen tropic compression, for high altitude hypersonic flight. The regime treated covers altitude from 100,000 feet to 400,000 feet in increments of 2000 feet, and a range of flight speeds from 10,000 to 25,000 feet per second. (Author).
Author: Richard W. Hales
Publisher:
ISBN:
Category : Gas dynamics
Languages : en
Pages : 78
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Book Description
