High-order semi-implicit schemes for unsteady compressible flow simulations

AIAA Journal

Volumn 40, Issue 5, 2002, Pages 869-878

  Dong, Haibo ^a   Zhong, Xiaolin ^a  

^a UNIVERSITY OF CALIFORNIA   (United States)

Author keywords

[No Author keywords available]

Indexed keywords

BOUNDARY LAYERS; COMPRESSIBLE FLOW; COMPUTER SIMULATION; NAVIER STOKES EQUATIONS; UNSTEADY FLOW; VISCOUS FLOW;

TRANSIENT FLOW;

COMPUTATIONAL FLUID DYNAMICS;

EID: 0036572669     PISSN: 00011452     EISSN: None     Source Type: Journal    
DOI: 10.2514/2.1753     Document Type: Article

References (14)

1. Numerical simulation of transition in wall-bounded shear flows
2. Numerical experiments in supersonic boundary-layer stability
3. Direct numerical simulation of transition in supersonic boundary layer: Oblique breakdown
4. Spatial numerical simulations of linear and weakly nonlinear instabilities in supersonic boundary layers
5. Subharmonic transition to turbulence in a flat-plate boundary layer at mach number 4.5
6. A comparision study of an improved temporal DNS and spatial DNS of compressible boundary layer transition
7. Additive semi-implicit runge-kutta schemes for computing high-speed nonequilibrium reactive flows
8. High-order finite-difference schemes for numerical simulation of hypersonic boundary layer transition
9. Low-storage semi-implicit runge-kutta methods for reactive flow computations
10. Boundary conditions for incompressible flows
11. Spectral multi-domain for large-scale fluid dynamic simulations
12. Boundary conditions for direct simulations of compressible viscous flows
13. A computational approach to swept leading-edge receptivity
14. Linear stability of viscous supersonic plane couette flow