Inviscid, Nonequilibrium Flow Behind Bow and Normal Shock Waves: The revised normal shock program, by Leonard J. Garr [and others] 1966 PDF Download

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Inviscid, Nonequilibrium Flow Behind Bow and Normal Shock Waves: The revised normal shock program, by Leonard J. Garr [and others] 1966

Inviscid, Nonequilibrium Flow Behind Bow and Normal Shock Waves: The revised normal shock program, by Leonard J. Garr [and others] 1966 PDF Author: Cornell Aeronautical Laboratory
Publisher:
ISBN:
Category : Shock waves
Languages : en
Pages : 144

Book Description


Inviscid, Nonequilibrium Flow Behind Bow and Normal Shock Waves: The revised normal shock program, by Leonard J. Garr [and others] 1966

Inviscid, Nonequilibrium Flow Behind Bow and Normal Shock Waves: The revised normal shock program, by Leonard J. Garr [and others] 1966 PDF Author: Cornell Aeronautical Laboratory
Publisher:
ISBN:
Category : Shock waves
Languages : en
Pages : 144

Book Description


Scientific and Technical Aerospace Reports

Scientific and Technical Aerospace Reports PDF Author:
Publisher:
ISBN:
Category : Aeronautics
Languages : en
Pages : 352

Book Description


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

Inviscid, Nonequilibrium Flow Behind Bow and Normal Shock Waves: General analysis and numerical examples, by P. V. Marrone PDF Author: Cornell Aeronautical Laboratory
Publisher:
ISBN:
Category : Shock waves
Languages : en
Pages : 120

Book Description


Inviscid, Nonequilibrium Flow Behind Bow and Normal Shock Waves: The IBM 704 computer programs, by L. J. Garr and P. V. Marrone

Inviscid, Nonequilibrium Flow Behind Bow and Normal Shock Waves: The IBM 704 computer programs, by L. J. Garr and P. V. Marrone PDF Author: Cornell Aeronautical Laboratory
Publisher:
ISBN:
Category : Shock waves
Languages : en
Pages : 0

Book Description


Inviscid, Nonequilibrium Flow Behind Bow and Normal Shock Waves

Inviscid, Nonequilibrium Flow Behind Bow and Normal Shock Waves PDF Author: Cornell Aeronautical Laboratory
Publisher:
ISBN:
Category : Shock waves
Languages : en
Pages : 0

Book Description


NASA Technical Note

NASA Technical Note PDF Author:
Publisher:
ISBN:
Category :
Languages : en
Pages : 596

Book Description


General Chemical Kinetics Computer Program for Static and Flow Reactions, with Application to Combustion and Shock-tube Kinetics

General Chemical Kinetics Computer Program for Static and Flow Reactions, with Application to Combustion and Shock-tube Kinetics PDF Author: David A. Bittker
Publisher:
ISBN:
Category : Chemical kinetics
Languages : en
Pages : 216

Book Description
A general chemical kinetics program is described for complex, homogeneous ideal-gas reactions in any chemical system. Its main features are flexibility and convenience in treating many different reaction conditions. The program solves numerically the differential equations describing complex reaction in either a static system or one-dimensional inviscid flow. Applications include ignition and combustion, shock wave reactions, and general reactions in a flowing or static system. An implicit numerical solution method is used which works efficiently for the extreme conditions of a very slow or a very fast reaction. The theory is described, and the computer program and users' manual are included.

חדושי רבינו אהרן הלוי

חדושי רבינו אהרן הלוי PDF Author:
Publisher:
ISBN:
Category :
Languages : en
Pages :

Book Description


Similitude for Normal Shock Waves in Nonequilibrium Flows

Similitude for Normal Shock Waves in Nonequilibrium Flows PDF Author: Ralph E. Thomas
Publisher:
ISBN:
Category : Shock waves
Languages : en
Pages : 60

Book Description
Similarity parameters are developed which govern the length of nonequilibrium zones behind normal shock waves. Non-equilibrium effects produced by both vibrational relaxation and dissociation are considered. The parameters can also account for arbitrary levels of free-stream vibrational energy or dissociation level. The validity of the parameters is examined using numerical computations of the properties of the non-equilibrium fields. These computations are made with the aid of experimentally based rate expressions. The parameters, when written in a form describing the variation of non-equilibrium zone length with Mach number, are shown to have acceptable accuracy. (Author).

The Inviscid Chemical Nonequlibrium Flow Behind a Moving Normal Shock Wave

The Inviscid Chemical Nonequlibrium Flow Behind a Moving Normal Shock Wave PDF Author: Dominic J. Palumbo
Publisher:
ISBN:
Category :
Languages : en
Pages : 31

Book Description
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).