![Inviscid, Nonequilibrium Flow Behind Bow and Normal Shock Waves: The revised normal shock program, by Leonard J. Garr [and others] 1966 PDF](https://books.google.com/books/content/images/frontcover/BZZTAAAAYAAJ?fife=w150-h200)
Author: Cornell Aeronautical LaboratoryPublisher:
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](https://books.google.com/books/content/images/frontcover/BZZTAAAAYAAJ?fife=w80-h100)
Author: Cornell Aeronautical LaboratoryPublisher:
ISBN:
Category : Shock waves
Languages : en
Pages : 144
Book Description
Inviscid, Nonequilibrium Flow Behind Bow and Normal Shock Waves: General analysis and numerical examples, by P. V. Marrone
Author: Cornell Aeronautical LaboratoryPublisher:
ISBN:
Category : Shock waves
Languages : en
Pages : 120
Book Description
Inviscid, Nonequilibrium Flow Behind Bow and Normal Shock Waves
Author: Cornell Aeronautical LaboratoryPublisher:
ISBN:
Category : Shock waves
Languages : en
Pages : 0
Book Description
Inviscid, Nonequilibrium Flow Behind Bow and Normal Shock Waves: The IBM 704 computer programs, by L. J. Garr and P. V. Marrone
Author: Cornell Aeronautical LaboratoryPublisher:
ISBN:
Category : Shock waves
Languages : en
Pages : 0
Book Description
Similitude for Normal Shock Waves in Nonequilibrium Flows
Author: Ralph E. ThomasPublisher:
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).
חדושי רבינו אהרן הלוי
Author: Inviscid, Nonequilibrium Flow Behind Bow and Normal Shock Waves
Author: Cornell University. Cornell Aeronautical Laboratory, IncPublisher:
ISBN:
Category :
Languages : en
Pages : 242
Book Description
The Inviscid Chemical Nonequlibrium Flow Behind a Moving Normal Shock Wave
Author: Dominic J. PalumboPublisher:
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).
A Thin-shock-layer Solution for Nonequilibrium, Inviscid Hypersonic Flows in Earth, Martian, and Venusian Atmospheres
Author: William L. GosePublisher:
ISBN:
Category : Inviscid flow
Languages : en
Pages : 164
Book Description
An approximate inverse solution is presented for the nonequilibrium flow in the inviscid shock layer about a vehicle in hypersonic flight. The method is based upon a thin-shock-layer approximation and has the advantage of being applicable to both subsonic and supersonic regions of the shock layer. The relative simplicity of the method makes it ideally suited for programming on a digital computer with a significant reduction in storage capacity and computing time required by other more exact methods. Comparison of nonequilibrium solutions for an air mixture obtained by the present method is made with solutions obtained by two other methods. Additional cases are presented for entry of spherical nose cones into representative Venusian and Martian atmospheres. A digital computer program written in FORTRAN language is presented that permits an arbitrary gas mixture to be employed in the solution. The effects of vibration, dissociation, recombination, electronic excitation, and ionization are included in the program.
An Estimate of the Chemical Kinetics Behind Normal Shock Waves in Mixtures of Carbon Dioxide and Nitrogen for Conditions of Mars Entry
Author: Robert L. McKenziePublisher:
ISBN:
Category : Carbon dioxide
Languages : en
Pages : 66
Book Description