A model for erosive burning of homogeneous propellants

Combustion and Flame

Volumn 157, Issue 2, 2010, Pages 397-407

  Zhang, Ju ^a   Jackson, Thomas L ^a  

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

Author keywords

Erosive burning; Modeling; Numerical simulations; Propellant

Indexed keywords

COMBUSTION RESPONSE; EROSIVE BURNING; FLAME STRETCH; HOMOGENEOUS SOLIDS; MODELING; MULTI SCALE ANALYSIS; NUMERICAL SIMULATION; UNDERLYING MECHANISM; VELOCITY FIELD;

COMPUTER SIMULATION; EXPLOSIVES; SOLID PROPELLANTS; SPACECRAFT PROPULSION;

COMBUSTION;

CHEMICAL PROPELLANT; INDUSTRIAL CHEMICAL; UNCLASSIFIED DRUG;

ARTICLE; CHEMICAL PHENOMENA; CHEMICAL REACTION; COMBUSTION; CONTROLLED STUDY; EROSIVE BURNING; FLAME; MATHEMATICAL MODEL; PRIORITY JOURNAL; VELOCITY;

EID: 73649115250     PISSN: 00102180     EISSN: None     Source Type: Journal    
DOI: 10.1016/j.combustflame.2009.09.008     Document Type: Article

References (42)

1. Green L. Erosive burning of some composite solid propellants. Jet Propul 24 (1954) 9-15
2. Marklund T., and Lake A. Experimental investigation of propellant erosion. ARS Journal 30 2 (1960) 173-178
3. Gordon J.C., Duterque J., and Lengelle G. Solid propellant erosive burning. J. Propul. Power 8 4 (1992) 741-747
4. Bulgakov V.K., Karpov A.I., and Lipanov A.M. Numerical studies of solid propellant erosive burning. J. Propul. Power 9 6 (1993) 812-818
5. Gordon J.C., Duterque J., and Lengelle G. Erosive burning in solid propellant motors. J. Propul. Power 9 6 (1993) 741-747
6. King M.K. Erosive burning of solid propellants. J. Propul. Power 9 6 (1993) 785-805
7. Furfaro J.A. Erosive burning study utilizing ultrasonic measurement techniques. AIAA Paper (2003) 2003-4806
8. Krishnan S., and Rajesh K.K. Erosive burning of ammonium perchlorate/hydroxyl-terminated-polybutadiene propellants under supersonic crossflows. J. Propul. Power 19 4 (2003) 741-747
9. Landsbaum E.M. Erosive burning of solid rocket propellants - a revisit. J. Propul. Power 21 3 (2005) 470-477
10. Moss J., Heister S., and Linke K. Experimental program to assess erosive burning in segmented solid rocket motors. AIAA Paper (2007) 2007-5782
11. Cai W., Thakre P., and Yang V. A model of AP/HTPB composite propellant combustion in rocket-motor environments. Combust. Sci. Technol. 180 12 (2008) 2143-2169
12. Cai W., Thakre P., and Yang V. Transient combustion response of AP/HTPB composite propellant to acoustic oscillations in a rocket motor. Combust. Sci. Technol. 181 4 (2009) 597-617
13. H. Tsuji, An aerothermochemical analysis of ersoive burning of solid propellants, in: Proceedings of the 9th International Symposium on Combustion, Williams & Wilkins, Baltimore, MD, 1963, pp. 384-393.
14. Vilyunov V.N., and Dvoryashin A.A. An experimental investigation of erosive burning effects. Combust. Explo. Shock Waves 7 1 (1971) 38-42
15. Vilyunov V.N., and Dvoryashin A.A. On the influence of the initial temperature of solid fuel on the effect of negative erosivity. Fizika Gorenia i Vzryva 9 4 (1973) 602
16. Beddini R.A. Reacting turbulent boundary-layer approach to solid propellant erosive burning. AIAA J. 16 9 (1978) 898-905
17. Beddini R.A. Aerothermochemical analysis of erosive burning in a laboratory solid-rocket motor. AIAA J. 18 11 (1980) 1346-1353
18. King M.K. Model for prediction of double-base propellant burn rate, including cross-flow effects. AIAA J. 20 10 (1982) 1432-1439
19. A. Ishihara, N. Kubota, Erosive burning mechanism of double-based propellants, in: Twenty-first Symposium (International) on Combustion, The Combustion Institute, 1986, pp. 1975-1981.
20. Bulgakov V.K., Larpov A.I., and Lipanov A.M. Numerical studies of solid propellant erosive burning. J. Propul. Power 9 6 (1993) 812-818
21. McDonald B.A., and Menon S. Direct numerical simulation of solid propellant combustion in crossflow. J. Propul. Power 21 3 (2005) 460-469
22. Taylor G.I. Fluid flow in regions bounded by porous surfaces. Proc. R. Soc. London, A 234 (1956) 456
23. Culick F.E.C. Rotational axisymmetric mean flow and damping of acoustic waves in solid propellant rocket motors. AIAA J. 4 (1966) 1462-1464
24. Flandro G.A. Effects of vorticity on rocket combustion stability. J. Propul. Power 11 4 (1995) 607-625
25. Roh T.S., Tseng I.S., and Yang V. Effects of acoustic oscillations on flame dynamics of homogeneous propellants in rocket motors. J. Propul. Power 11 4 (1995) 640-650 (Value of shear rate provided by V. Yang, private communication)
26. Zhao Q., Staab P.L., Kassoy D.R., and Kirkkopru K. Acoustically generated vorticity in an internal flow. J. Fluid Mech. 413 (2000) 247-285
27. Buckmaster J., and Jackson T.L. The effects of time-periodic shear on a diffusion flame anchored to a propellant. Combust. Flame 120 (2000) 211-221
28. Isfahani A.H.G., Zhang J., and Jackson T.L. The effects of turbulence-induced time-periodic shear on a flame anchored to a propellant. Combust. Flame 156 (2009) 1084-1098
29. Beckstead M.W., Derr R.L., and Price C.F. A model of composite solid-propellant combustion based on multiple flames. AIAA J. 8 12 (1970) 2200-2207
30. P. Venugopal, F.M. Najjar, R.D. Moser, DNS and LES computations of model solid rocket motors. in: AIAA-2000-3571, 36th AIAA/ASME/SAE/ASEE Joint Propulsion Conference and Exhibit, Huntsville, AL, July 16-19, 2000.
31. P. Venugopal, F.M. Najjar, R.D. Moser, Numerical simulations of model solid rocket motor flows. in: AIAA Paper 2001-3950, 37th AIAA/ASME/SAE/ASEE Joint Propulsion Conference and Exhibit, Salt Lake City, UT, July 8-11, 2001.
32. P. Venugopal, Direct Numerical Simulation of Turbulence in a Model Solid Rocket Motor. PhD Thesis, University of Illinois at Urbana-Champaign, 2003.
33. Venugopal P., Moser R.D., and Najjar F.M. Direct numerical simulation of turbulence in injection driven plane channel flows. Phys. Fluids 20 (2008) 105103
34. Buckmaster J.D., and Ludford G.S.S. Theory of Laminar Flames (1982), Cambridge University Press, Cambridge
35. θ = 1410. J. Fluid Mech. 187 (1988) 61-98
36. Zhang J., and Jackson T.L. A high-order incompressible flow solver with WENO. J. Comput. Phys. 228 (2009) 2426-2442
37. Jiang G.S., and Shu C.W. Efficient implementation of weighted ENO schemes. J. Comput. Phys. 126 (1996) 202
38. Lele S.K. Compact finite differences with spectral like resolution. J. Comput. Phys. 103 (1992) 16
39. Kim J., and Moin P. Applications of a fractional-step method to incompressible Navier-Stokes equations. J. Comput. Phys. 59 (1985) 308-323
40. Hu F.Q., Hussaini M.Y., and Manthey J.L. Low-dissipation and -dispersion Runge-Kutta schemes for computational acoustics. J. Comput. Phys. 124 (1996) 177-191
41. Flandro G.A., and Majdalani J. Aeroacoustic instability in rockets. AIAA J. 41 3 (2003) 485-497
42. Balakrishnan G., Linan A., and Williams F.A. Rotational inviscid flow in laterally burning solid-propellant rocket motors. J. Propul. Power 8 6 (1992) 1167-1176