Numerical simulation of blast flowfields using a high resolution TVD finite volume scheme

Computers and Fluids

Volumn 18, Issue 1, 1990, Pages 103-137

  Wang, J C T ^a   Widhopf, G F ^a  

^a AEROSPACE CORPORATION   (United States)

Author keywords

[No Author keywords available]

Indexed keywords

FLOW OF FLUIDS; GAS DYNAMICS; ROCKETS AND MISSILES--LAUNCHING; SHOCK TUBES; SHOCK WAVES;

BLAST FLOW ENVIRONMENT; BLAST FLOWFIELDS; NUMERICAL SIMULATION; TOTAL VARIATION DIMINISHING (TVD) FINITE VOLUME INVISCID SCHEMES; WEAPON FIRING;

BLASTING;

EID: 0025556247     PISSN: 00457930     EISSN: None     Source Type: Journal    
DOI: 10.1016/0045-7930(90)90005-I     Document Type: Article

References (18)

1. Time-dependent near field muzzle brake flow simulations
2. Three-dimensional simulation of muzzle brake flow-fields
3. Three-dimensional simulation of STS ignition overpressure
4. A computational scheme for two-dimensional non-stationary problems of gas dynamics and calculation of the flow from a shock wave approaching a stationary state
5. Computation of the space shuttle solid rocket booster start-up transient flow
6. Numerical investigation of unsteady flow development in a nozzle-duct configuration
7. Blast computation using Harten's total variation diminishing scheme
8. Blast flowfield simulations
9. Implicit total variation diminishing (TVD) schemes for steady-state calculations
10. Numerical simulation by TVD schemes of complex shock reflections from airfoils at angle of attack
11. A high-resolution TVD finite volume scheme for the Euler equations in conservative form
12. High resolution schemes for hyperbolic conservation laws
13. Approximate Riemann solvers, parameter vectors and difference schemes
14. Noise from shock tube facilities
15. The perturbed region behind a diffracting shock wave