Unsteady dynamic variables method for heterogeneous solid propellant burning

AIAA Journal

Volumn 39, Issue 12, 2001, Pages 2343-2350

  Surzhikov, S T ^b   Krier, Herman ^a,c  

^a UNIVERSITY OF ILLINOIS AT URBANA CHAMPAIGN   (United States)

^b INSTITUTE FOR PROBLEMS IN MECHANICS   (Russian Federation)

^c University of Illinois at Urbana Champaign   (United States)

Author keywords

[No Author keywords available]

Indexed keywords

COMBUSTION; COMPUTATIONAL FLUID DYNAMICS; COMPUTER SIMULATION; DENSITY (SPECIFIC GRAVITY); GRAVITATIONAL EFFECTS; MATHEMATICAL MODELS; NAVIER STOKES EQUATIONS; SUBSONIC AERODYNAMICS; THERMAL EFFECTS; UNSTEADY FLOW; VORTEX FLOW;

MULTICOMPONENT BURNING;

SOLID PROPELLANTS;

EID: 0035668318     PISSN: 00011452     EISSN: None     Source Type: Journal    
DOI: 10.2514/2.1240     Document Type: Article

References (11)

1. Numerical simulation of low-speed unsteady wake development behind airfoils, using incompressible and compressible analyses
2. 2D model for unsteady burning of heterogeneous AP/binder solid propellants
3. Study of flame structure for mixed solid fuels based on ammonium perchlorate and polybutadiene rubber
4. Nonpremixed periodic flames supported by heterogeneous propellants
5. Two-dimensional combustion modeling of heterogeneous solid propellants with finite peclet number
6. Combustion of ammonium perchlorate-polymer sandwiches