Method for Calculating Effects of Dissociation on Flow Variables in the Relaxation Zone Behind Normal Shock Waves

Method for Calculating Effects of Dissociation on Flow Variables in the Relaxation Zone Behind Normal Shock Waves PDF Author: John S. Evans
Publisher:
ISBN:
Category : Air flow
Languages : en
Pages : 668

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Book Description
Because the chemical reaction rates needed to predict the dependence of degree of dissociation on distance behind the shock are not known, order-of-magnitude estimates of their values have been used in a numerical example, the purpose of which is to illustrate the use of reaction-rate equations to predict relaxation time and distance behind the shock front.

Method for Calculating Effects of Dissociation on Flow Variables in the Relaxation Zone Behind Normal Shock Waves

Method for Calculating Effects of Dissociation on Flow Variables in the Relaxation Zone Behind Normal Shock Waves PDF Author: John S. Evans
Publisher:
ISBN:
Category : Air flow
Languages : en
Pages : 668

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Book Description
Because the chemical reaction rates needed to predict the dependence of degree of dissociation on distance behind the shock are not known, order-of-magnitude estimates of their values have been used in a numerical example, the purpose of which is to illustrate the use of reaction-rate equations to predict relaxation time and distance behind the shock front.

A Technique for Determining Relaxation Times by Free-Flight Tests of Low-Fineness-Ratio Cones; With Experimental Results for Air at Equilibrium Temperatures Up to 3440 K

A Technique for Determining Relaxation Times by Free-Flight Tests of Low-Fineness-Ratio Cones; With Experimental Results for Air at Equilibrium Temperatures Up to 3440 K PDF Author: Jack D. Stephenson
Publisher:
ISBN:
Category : Photography, Shadowgraph
Languages : en
Pages : 64

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This report describes a technique which combines theory and experiments for determining relaxation times in gases. The technique is based on the measurement of shapes of the bow shock waves of low-fineness-ratio cones fired from high-velocity guns. The theory presented in the report provides a means by which shadowgraph data showing the bow waves can be analyzed so as to furnish effective relaxation times. Relaxation times in air were obtained by this technique and the results have been compared with values estimated from shock tube measurements in pure oxygen and nitrogen. The tests were made at velocities ranging from 4600 to 12,000 feet per second corresponding to equilibrium temperatures from 35900 R (19900 K) to 6200 R (34400 K), under which conditions, at all but the highest temperatures, the effective relaxation times were determined primarily by the relaxation time for oxygen and nitrogen vibrations.

Effects of Chemical Dissociation and Molecular Vibrations on Steady One-dimensional Flow

Effects of Chemical Dissociation and Molecular Vibrations on Steady One-dimensional Flow PDF Author: Steve Paul Heims
Publisher:
ISBN:
Category : Dissociation
Languages : en
Pages : 72

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Effects of Chemical Dissociation and Molecular Vibrations on Steady One-dimensional Flow

Effects of Chemical Dissociation and Molecular Vibrations on Steady One-dimensional Flow PDF Author: Steve P. Heims
Publisher:
ISBN:
Category : Dissociation
Languages : en
Pages : 76

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Technical Note

Technical Note PDF Author:
Publisher:
ISBN:
Category : Aeronautics
Languages : en
Pages : 468

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Technical Note - National Advisory Committee for Aeronautics

Technical Note - National Advisory Committee for Aeronautics PDF Author: United States. National Advisory Committee for Aeronautics
Publisher:
ISBN:
Category : Aeronautics
Languages : en
Pages : 986

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Measurements of the Dissociation Rate of Molecular Oxygen

Measurements of the Dissociation Rate of Molecular Oxygen PDF Author: Charles J. Schexnayder
Publisher:
ISBN:
Category : Dissociation
Languages : en
Pages : 28

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Book Description
The ability of molecular oxygen to absorb light in the Schumann-Runge ultraviolet region of the spectrum has been used to follow the change in concentration of molecular oxygen as a function of time behind shock waves in oxygen and in a mixture of 10-percent oxygen in argon. Analysis of the records obtained yielded values for the dissociation rate of oxygen as a function of temperature over the range 4,000° to 10,000°K. The highest previously reported experimental results in the literature were at 7,500°K.

NASA Technical Report

NASA Technical Report PDF Author:
Publisher:
ISBN:
Category : Aerodynamics
Languages : en
Pages : 722

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NASA Technical Note

NASA Technical Note PDF Author:
Publisher:
ISBN:
Category :
Languages : en
Pages : 430

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Handbook of Supersonic Aerodynamics

Handbook of Supersonic Aerodynamics PDF Author: I. I. Glass
Publisher:
ISBN:
Category : Aerodynamics, Supersonic
Languages : en
Pages : 642

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