A Numerical Simulation of a 2D- Viscous Hypersonic Flow Using the Time-Marching Method of Characteristics

Notes on Numerical Fluid Mechanics (NNFM) - New Results in Numerical and Experimental Fluid Mechanics II ◽

10.1007/978-3-663-10901-3_48 ◽

1999 ◽

pp. 371-378

Author(s):

H. Sanaknaki ◽

J. Ballmann

Keyword(s):

Numerical Simulation ◽

Hypersonic Flow ◽

Method Of Characteristics ◽

Time Marching ◽

Viscous Hypersonic Flow ◽

Marching Method

Download Full-text

A multi-dimensional time-marching method of characteristics for viscous and heat-conducting flows

Archive of Applied Mechanics ◽

10.1007/s004199900038 ◽

2000 ◽

Vol 70 (1-3) ◽

pp. 65-80

Author(s):

J. Ballmann ◽

H. Sanaknaki

Keyword(s):

Method Of Characteristics ◽

Heat Conducting ◽

Time Marching ◽

Marching Method

Download Full-text

Numerical Simulation of the Effect of Porous Cooling of Bodies in Hypersonic Flow

Heat Transfer Research ◽

10.1615/heattransres.v33.i1-2.90 ◽

2002 ◽

Vol 33 (1-2) ◽

pp. 8

Author(s):

Alexander I. Leontiev ◽

V. V. Nosatov ◽

G. S. Sadovnikov

Keyword(s):

Numerical Simulation ◽

Hypersonic Flow

Download Full-text

An investigation of two-dimensional flows of nucleating and wet steam by the time-marching method

International Journal of Heat and Fluid Flow ◽

10.1016/0142-727x(80)90003-x ◽

1980 ◽

Vol 2 (1) ◽

pp. 5-18 ◽

Cited By ~ 73

Author(s):

F. Bakhtar ◽

M.T. Mohammadi Tochai

Keyword(s):

Two Dimensional ◽

Wet Steam ◽

Time Marching ◽

Marching Method ◽

Two Dimensional Flows

Download Full-text

Calculation of the Quasi Three-Dimensional Flow in a Turbomachine Blade Row

Journal of Engineering for Power ◽

10.1115/1.3446252 ◽

1977 ◽

Vol 99 (1) ◽

pp. 53-62 ◽

Cited By ~ 1

Author(s):

Jean-Pierre Veuillot

Keyword(s):

Finite Difference ◽

Three Dimensional ◽

Three Dimensional Flow ◽

Through Flow ◽

Blade Row ◽

Time Marching ◽

Space Discretization ◽

Finite Volume Approach ◽

Marching Method ◽

Finite Difference Techniques

The equations of the through flow are obtained by an asymptotic theory valid when the blade pitch is small. An iterative method determines the meridian stream function, the circulation, and the density. The various equations are discretized in an orthogonal mesh and solved by classical finite difference techniques. The calculation of the steady transonic blade-to-blade flow is achieved by a time marching method using the MacCormack scheme. The space discretization is obtained either by a finite difference approach or by a finite volume approach. Numerical applications are presented.

Download Full-text