Exact Solutions of Reflected Normal Shock-wave Flow Fields with Nonequilibrium Chemical Reactions

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ISBN 13 :
Total Pages : 10 pages
Book Rating : 4.:/5 (44 download)

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Book Synopsis Exact Solutions of Reflected Normal Shock-wave Flow Fields with Nonequilibrium Chemical Reactions by : Leroy L. Presley

Download or read book Exact Solutions of Reflected Normal Shock-wave Flow Fields with Nonequilibrium Chemical Reactions written by Leroy L. Presley and published by . This book was released on 1968 with total page 10 pages. Available in PDF, EPUB and Kindle. Book excerpt:

Numerical Solutions of Several Reflected Shock-wave Flow Fields with Nonequilibrium Chemical Reactions

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ISBN 13 :
Total Pages : 60 pages
Book Rating : 4.:/5 (31 download)

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Book Synopsis Numerical Solutions of Several Reflected Shock-wave Flow Fields with Nonequilibrium Chemical Reactions by : Ronald K. Hanson

Download or read book Numerical Solutions of Several Reflected Shock-wave Flow Fields with Nonequilibrium Chemical Reactions written by Ronald K. Hanson and published by . This book was released on 1972 with total page 60 pages. Available in PDF, EPUB and Kindle. Book excerpt: The method of characteristics for a chemically reacting gas is used in the construction of the time-dependent, one-dimensional flow field resulting from the normal reflection of an incident shock wave at the end wall of a shock tube. Nonequilibrium chemical reactions are allowed behind both the incident and reflected shock waves. All the solutions are evaluated for oxygen, but the results are generally representative of any inviscid, nonconducting, and nonradiating diatomic gas. The solutions clearly show that: (1) both the incident- and reflected-shock chemical relaxation times are important in governing the time to attain steady state thermodynamic properties; and (2) adjacent to the end wall, an excess-entropy layer develops wherein the steady state values of all the thermodynamic variables except pressure differ significantly from their corresponding Rankine-Hugoniot equilibrium values.

Inviscid, Nonequilibrium Flow Behind Bow and Normal Shock Waves: General analysis and numerical examples, by P. V. Marrone

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ISBN 13 :
Total Pages : 120 pages
Book Rating : 4.E/5 ( download)

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Book Synopsis Inviscid, Nonequilibrium Flow Behind Bow and Normal Shock Waves: General analysis and numerical examples, by P. V. Marrone by : Cornell Aeronautical Laboratory

Download or read book Inviscid, Nonequilibrium Flow Behind Bow and Normal Shock Waves: General analysis and numerical examples, by P. V. Marrone written by Cornell Aeronautical Laboratory and published by . This book was released on 1965 with total page 120 pages. Available in PDF, EPUB and Kindle. Book excerpt:

Chemical Non-equilibrium Shock Flow

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ISBN 13 :
Total Pages : 70 pages
Book Rating : 4.E/5 ( download)

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Book Synopsis Chemical Non-equilibrium Shock Flow by : V. A. Langelo

Download or read book Chemical Non-equilibrium Shock Flow written by V. A. Langelo and published by . This book was released on 1963 with total page 70 pages. Available in PDF, EPUB and Kindle. Book excerpt: The problem of calculating the flow behind a normal shock front is discussed. The additional complication of finite reaction rate chemistry has been included. A numerical method and several results of flow across a shock wave with an eleven-species, thirteen reaction model of air are presented. Results of the method are discussed and compared with those of Hall, Escheroeder, and Marrone (inviscid hypersonic air flows with coupled non-equilibrium processes. IAS 30th annual meeting, Jan 1962). (Author).

Non-equilibrium Flow Fields with Chemical Reactions in a Shock Tube

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ISBN 13 :
Total Pages : 78 pages
Book Rating : 4.:/5 (227 download)

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Book Synopsis Non-equilibrium Flow Fields with Chemical Reactions in a Shock Tube by : Elihu Zimet

Download or read book Non-equilibrium Flow Fields with Chemical Reactions in a Shock Tube written by Elihu Zimet and published by . This book was released on 1969 with total page 78 pages. Available in PDF, EPUB and Kindle. Book excerpt: The two chemical reactions given by N2O4 + M = 2NO2 + M = 2NO + O2 + M, where M represents the inert carrier gases argon or nitrogen, were studied. The experiments were carried out in a temperature controlled shock tube and a light absorption technique permitted the time dependent concentration of the species NO2 to be determined. For shock strengths where the temperature did not exceed 400K only the first chemical reaction took place. Stronger shock waves excited both chemical reactions with temperatures up to 2100K, and for this reason, flow fields with two nonequilibrium modes could be investigated. Since the relaxation times of these two reactions were different by about three orders of magnitude, they could be experimentally uncoupled. A study of the reaction mechanisms and rate constants for both reactions was carried out. At shock strengths exciting only the first chemical reaction the complete picture of a non-equilibrium flow field with only one nonequilibrium mode could be investigated. In this situation, the shock strengths were varied from weak, fully dispersed waves to strong, partly dispersed waves. (Author).

Nonequilibrium Flow Fields Behind Reflected Shock Waves

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ISBN 13 :
Total Pages : 296 pages
Book Rating : 4.:/5 (259 download)

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Book Synopsis Nonequilibrium Flow Fields Behind Reflected Shock Waves by : Harold Joseph Brandon

Download or read book Nonequilibrium Flow Fields Behind Reflected Shock Waves written by Harold Joseph Brandon and published by . This book was released on 1969 with total page 296 pages. Available in PDF, EPUB and Kindle. Book excerpt:

Reflection of a Weak Shock Wave with Vibrational Relaxation from a Wall

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ISBN 13 :
Total Pages : 212 pages
Book Rating : 4.E/5 ( download)

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Book Synopsis Reflection of a Weak Shock Wave with Vibrational Relaxation from a Wall by : Ching-mao Hung

Download or read book Reflection of a Weak Shock Wave with Vibrational Relaxation from a Wall written by Ching-mao Hung and published by . This book was released on 1972 with total page 212 pages. Available in PDF, EPUB and Kindle. Book excerpt:

Applied Mechanics Reviews

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ISBN 13 :
Total Pages : 568 pages
Book Rating : 4.:/5 (26 download)

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Book Synopsis Applied Mechanics Reviews by :

Download or read book Applied Mechanics Reviews written by and published by . This book was released on 1972 with total page 568 pages. Available in PDF, EPUB and Kindle. Book excerpt:

Numerical Results for the Diffraction of a Normal Shock Wave by a Sphere and for the Subsequent Transient Flow

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ISBN 13 :
Total Pages : 44 pages
Book Rating : 4.:/5 (317 download)

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Book Synopsis Numerical Results for the Diffraction of a Normal Shock Wave by a Sphere and for the Subsequent Transient Flow by : Richard W. Barnwell

Download or read book Numerical Results for the Diffraction of a Normal Shock Wave by a Sphere and for the Subsequent Transient Flow written by Richard W. Barnwell and published by . This book was released on 1967 with total page 44 pages. Available in PDF, EPUB and Kindle. Book excerpt:

NASA Technical Note

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ISBN 13 :
Total Pages : 736 pages
Book Rating : 4.3/5 (91 download)

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Book Synopsis NASA Technical Note by :

Download or read book NASA Technical Note written by and published by . This book was released on 1973 with total page 736 pages. Available in PDF, EPUB and Kindle. Book excerpt:

Scientific and Technical Aerospace Reports

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ISBN 13 :
Total Pages : 1028 pages
Book Rating : 4.3/5 (91 download)

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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 1028 pages. Available in PDF, EPUB and Kindle. Book excerpt: Lists citations with abstracts for aerospace related reports obtained from world wide sources and announces documents that have recently been entered into the NASA Scientific and Technical Information Database.

Solution Procedure for Real Gas Shock Waves

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ISBN 13 :
Total Pages : 18 pages
Book Rating : 4.:/5 (227 download)

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Book Synopsis Solution Procedure for Real Gas Shock Waves by : L. Wassner

Download or read book Solution Procedure for Real Gas Shock Waves written by L. Wassner and published by . This book was released on 1971 with total page 18 pages. Available in PDF, EPUB and Kindle. Book excerpt: A numerical solution procedure is derived for one-dimensional stationary 'real gas flow' across a normal shock wave and in the wake of this wave. The following phenomena are taken into account: Non-equilibrium chemical reactions between diatomic and atomic species; non-equilibrium of the innermolecular energies of rotation and of vibration; transport of momentum, mass, and energy due to viscosity, thermal conductivity, mass diffusivity, and thermal diffusivity. (Author).

The Effect of Species Diffusion and Heat Conduction on Nonequilibrium Flows Behind Strong Shocks

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ISBN 13 :
Total Pages : 118 pages
Book Rating : 4.E/5 ( download)

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Book Synopsis The Effect of Species Diffusion and Heat Conduction on Nonequilibrium Flows Behind Strong Shocks by : Walter E. Gibson

Download or read book The Effect of Species Diffusion and Heat Conduction on Nonequilibrium Flows Behind Strong Shocks written by Walter E. Gibson and published by . This book was released on 1963 with total page 118 pages. Available in PDF, EPUB and Kindle. Book excerpt:

חדושי רבינו אהרן הלוי

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ISBN 13 :
Total Pages : pages
Book Rating : 4.:/5 (762 download)

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Book Synopsis חדושי רבינו אהרן הלוי by :

Download or read book חדושי רבינו אהרן הלוי written by and published by . This book was released on 1956 with total page pages. Available in PDF, EPUB and Kindle. Book excerpt:

International Aerospace Abstracts

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ISBN 13 :
Total Pages : 490 pages
Book Rating : 4.3/5 (91 download)

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Book Synopsis International Aerospace Abstracts by :

Download or read book International Aerospace Abstracts written by and published by . This book was released on 1995 with total page 490 pages. Available in PDF, EPUB and Kindle. Book excerpt:

The Inviscid Chemical Nonequlibrium Flow Behind a Moving Normal Shock Wave

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ISBN 13 :
Total Pages : 31 pages
Book Rating : 4.:/5 (227 download)

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Book Synopsis The Inviscid Chemical Nonequlibrium Flow Behind a Moving Normal Shock Wave by : Dominic J. Palumbo

Download or read book The Inviscid Chemical Nonequlibrium Flow Behind a Moving Normal Shock Wave written by Dominic J. Palumbo and published by . This book was released on 1968 with total page 31 pages. Available in PDF, EPUB and Kindle. Book excerpt: A time-dependent numerical scheme is used to solve for the chemical nonequilibrium profile a normal shock wave in air. The steady state equations are also integrated using a fourth order Runge-Kutta technique and a comparison is made with the time-dependent calculation. The results agree within one percent except in the region close to the shock. In this region the profiles differ because the time-dependent technique allows calculation through the shock (which is several mesh points in width) and as a result some dissociation occurs. (Author).

Exact and Approximate Solutions to the Oblique Shock Equations for Real-Time Applications

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Publisher : Independently Published
ISBN 13 : 9781792601293
Total Pages : 26 pages
Book Rating : 4.6/5 (12 download)

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Book Synopsis Exact and Approximate Solutions to the Oblique Shock Equations for Real-Time Applications by : National Aeronautics and Space Adm Nasa

Download or read book Exact and Approximate Solutions to the Oblique Shock Equations for Real-Time Applications written by National Aeronautics and Space Adm Nasa and published by Independently Published. This book was released on 2018-12-29 with total page 26 pages. Available in PDF, EPUB and Kindle. Book excerpt: The derivation of exact solutions for determining the characteristics of an oblique shock wave in a supersonic flow is investigated. Specifically, an explicit expression for the oblique shock angle in terms of the free stream Mach number, the centerbody deflection angle, and the ratio of the specific heats, is derived. A simpler approximate solution is obtained and compared to the exact solution. The primary objectives of obtaining these solutions is to provide a fast algorithm that can run in a real time environment. Hartley, T. T. and Brandis, R. and Mossayebi, F. NASA-CR-187173, NAS 1.26:187173 NAG3-904; RTOP 505-62-40...