Transient Combustion Response of AP/HTPB Composite Propellant to Acoustic Oscillations in a Rocket Motor

REFERENCES

• Apte , S. , and Yang , V. 2002 . Unsteady flow evolution in porous chamber with surface mass injection, Part 2: Acoustic excitation . AIAA Journal , 40 , 244 .
   Web of Science ®Google Scholar
• Baum , J.D. , and Levine , J.N. 1986 . Modeling of nonlinear longitudinal instability in solid rocket motors . Acta Astronautica , 13 , 339 .
   Web of Science ®Google Scholar
• Brewster , M.Q. , and Son , S.F. 1995 . Quasi-steady combustion modeling of homogeneous solid propellants . Combustion and Flame , 103 , 11 .
   Web of Science ®Google Scholar
• Brewster , M.Q. , Ward , M.J. , and Son , S.F. 2000 . Quasi-steady combustion modeling of homogeneous solid propellants . Combustion Science and Tech. , 154 , 1 .
   Web of Science ®Google Scholar
• Cai , W. , Ma , F.H. , and Yang , V. 2003 . Two-phase flow interactions in solid-propellant rocket motors with acoustic oscillations . Journal of Propulsion and Power , 19 , 385 .
   Web of Science ®Google Scholar
• Cai , W. , Thakre , P. , and Yang , V. 2008 . A model of AP/HTPB composite propellant combustion in rocket motor environments . Combustion Science and Tech. , 180 , 2143 .
   Web of Science ®Google Scholar
• Chu , W.-W. , Yang , V. , and Majdalani , J. 2003. Premixed flame response to acoustic waves in a porous-walled chamber with surface mass injection. Combustion and Flame , 133, 359.
   Web of Science ®Google Scholar
• Cohen , N.S. , and Strand , L.D. 1985a . Combustion response to compositional fluctuations . AIAA Journal , 23 , 760 .
   Web of Science ®Google Scholar
• Cohen , N.S. , and Strand , L.D. 1985b . Effects of AP particle size on combustion response to cross flow . AIAA Journal , 23 , 776 .
   Web of Science ®Google Scholar
• Culick , F.E.C. 1968 . A review of calculations for unsteady burning of a solid propellant . AIAA Journal , 6 , 2241 .
   Web of Science ®Google Scholar
• Culick , F.E.C. , and Yang , V. 1992 . Prediction of the stability of unsteady motions in solid propellant rocket motors . In De Luca , L. , Price , E.W. , and Summerfield , M. (Eds.), Nonsteady burning and combustion stability of solid propellants , vol. 143 . Progress in Astronautics and Aeronautics, AIAA, 719 , Washington , DC .
   Google Scholar
• Flandro , G.A. 1995 . Effects of vorticity on rocket combustion stability . Journal of Propulsion and Power , 11 , 607 .
   Web of Science ®Google Scholar
• Flandro , G.A. , Cai , W. , and Yang , V. 2000 . Turbulent transport in rocket motor unsteady flowfield . In Yang , V. , Brill , T.B. , and Ren , W.Z. (Eds.), Solid propellant chemistry, combustion and motor interior ballistics , vol. 185 . Progress in Astronautics and Aeronautics, AIAA, 837 , New York .
   Google Scholar
• Guirao , C. , and Williams , F.A. 1971 . A model for aluminum perchlorate deflagration between 20 and 100 atm . AIAA Journal , 9 , 1345 .
   Web of Science ®Google Scholar
• Hsieh , S.Y. , and Yang , V. 1997 . A preconditioned flux-differencing scheme for chemically reacting flows at all mach numbers . J. Comp. Fluid Dyn., 8 , 31 .
   Web of Science ®Google Scholar
• Levine , J.N. , and Baum , J.D. 1983 . Numerical study of nonlinear instability phenomenon in solid rocket motors . AIAA Journal , 21 , 557 .
   Web of Science ®Google Scholar
• Majdalani , J. 1999 . The boundary layer structure in cylindrical rocket motors . AIAA Journal , 37 , 505 .
   Web of Science ®Google Scholar
• Majdalani , J. , and Roh , T.S. 2000 . The oscillatory channel flow with large wall injection . Proceedings of the Royal Society, London, Series A , 456 , 1625 .
   Web of Science ®Google Scholar
• Majdalani , J. , and Van Moorhem , W.K. 1997 . A multiple-scales solution to the acoustic boundary layer in solid rocket motors . Journal of Propulsion and Power , 13 , 186 .
   Web of Science ®Google Scholar
• Marble , F.E. 1985 . Growth of a diffusion flame in the field of a vortex. In Casci , C. (Ed.), Recent advances in the aerospace science – In honor of Luigi Crocco on his seventy-fifth birthday , Plenum Prenum , New York , pp. 395 – 414 .
   Google Scholar
• Novozhilov , B.V. 1965 . Burning of a powder under harmonically varying pressure . Journal of Appl. Mech. Tech. Phys. , 6 , 103 .
   Google Scholar
• Pierce , A.D. 1989 . Acoustics: An introduction to its physical principles and applications . The Acoustical Society of America , New York .
   Google Scholar
• Roh , T.S. , Apte , S.V. , and Yang , V. 1998 . Transient combustion response of homogeneous solid propellant to acoustic oscillations in a rocket motor . Proceedings of the Combustion Institute , 27 , 1381 .
   Google Scholar
• Tseng , L.S. , and Yang , V. 1994 . Combustion of a double-base homogeneous propellant in a rocket motor . Combustion and Flame , 96 , 325 .
   Web of Science ®Google Scholar
• Wicker , J.M. , Greene , W.D. , Kim , S.-I. , and Yang , V. 1996 . Triggering of longitudinal combustion instabilities in rocket motors: Nonlinear combustion response . Journal of Propulsion and Power , 12 , 1148 .
   Web of Science ®Google Scholar
• Zong , N. , and Yang , V. 2007 . An efficient preconditioning scheme for general fluid mixtures using primitive pressure-temperature variables . International Journal of Computational Fluid Dynamics , 21 , 217 .
   Web of Science ®Google Scholar
• Zong , N. , and Yang , V. 2008 . Cryogenic fluid dynamics of pressure swirl injectors at supercritical conditions . Physics of Fluids , 20 , 056103 .
   Web of Science ®Google Scholar