A two-point difference scheme for computing steady-state solutions to the conservative one-dimensional Euler equations

Computers and Fluids

Volumn 12, Issue 1, 1984, Pages 11-30

  Wornom, Stephen F ^a  

^a NASA LANGLEY RESEARCH CENTER   (United States)

Author keywords

[No Author keywords available]

Indexed keywords

COMPUTER PROGRAMMING - ALGORITHMS; MATHEMATICAL TECHNIQUES - FINITE DIFFERENCE METHOD; SHOCK WAVES;

EULER EQUATIONS;

FLOW OF FLUIDS;

EID: 0021124472     PISSN: 00457930     EISSN: None     Source Type: Journal    
DOI: 10.1016/0045-7930(84)90024-0     Document Type: Article

References (11)

1. Acceleration of transonic potential flow calculations on arbitrary meshes by the multiple grid method
2. Comment on stability aspects of diverging subsonic flows
3. Stability aspects of diverging subsonic flow
4. Stable boundary approximations for a class of implicit schemes for the one-dimensional inviscid equations of gas dynamics
5. Artificial compressibility methods for numerical solutions of transonic full potential equation
6. Fast conservative schemes for the full potential equation applied to transonic flows
7. Steady shock tracking and Newton's method applied to one-dimensional duct flow
8. Implicit characteristic modelling schemes for the Euler equations—A new approach
9. A fast finite element method for transonic potential flow calculations
10. Compact difference schemes for mixed initial boundary value problems—I