Higher Flowfield Approximations for Solid Rocket Motors with Tapered Bores
暂无分享,去创建一个
[1] S. Balachandar,et al. Direct and Large Eddy Simulations of Compressible Wall-Injection Flows in Laminar, Transitional, and Turbulent Regimes , 2002 .
[2] Grégoire Casalis,et al. On the nonparallel stability of the injection induced two-dimensional Taylor flow , 2001 .
[3] Fred E. C. Culick,et al. Rotational axisymmetric mean flow and damping of acoustic waves in asolid propellant rocket. , 1966 .
[4] Gary A. Flandro,et al. Aeroacoustic Instability in Rockets , 2003 .
[5] G. Flandro,et al. On the origin of the DC shift , 1997 .
[6] J. Majdalani,et al. The oscillatory pipe flow with arbitrary wall injection , 2002, Proceedings of the Royal Society of London. Series A: Mathematical, Physical and Engineering Sciences.
[7] Gary A. Flandro,et al. Nonlinear Rocket Motor Stability Prediction: Limit Amplitude, Triggering, and Mean , 2004 .
[8] Curtis Clayton,et al. Flow fields in solid rocket motors with tapered bores , 1996 .
[9] Particle Effects on Solid-Propellant Motors Flow Stability , 2002 .
[10] H. Gibeling,et al. Navier-Stokes analysis of solid propellant rocket motor internal flows , 1989 .
[11] D. Couton,et al. Numerical simulation of vortex-shedding phenomenon in a channel with flow induced through porous wall , 1997 .
[12] J. Majdalani,et al. Higher Mean-Flow Approximation for Solid Rocket Motors with Radially Regressing Walls , 2002 .
[13] J. Majdalani,et al. Nonlinear Longitudinal Mode Instability in Liquid Propellant Rocket Engine Preburners , 2004 .
[14] Francois Vuillot,et al. Parietal vortex shedding as a cause of instability for long solid propellant motors - Numerial simulations and comparisons with firing tests , 1996 .
[15] R. Moser,et al. Numerical simulations of model solid rocket motor flows , 2001 .
[16] G. Casalis,et al. Spatial instability of flow in a semiinfinite cylinder with fluid injection through its porous walls , 2000 .
[17] Francois Vuillot,et al. Numerical simulations of parietal vortex-shedding phenomenon in a cold flow set-up , 1998 .
[18] J. Majdalani,et al. Improved Time-Dependent Flowfield Solution for Solid Rocket Motors , 1998 .
[19] Said Elghobashi,et al. On predicting particle-laden turbulent flows , 1994 .
[20] Robert D. Moser,et al. DNS and LES computations of model solid rocket motors , 2000 .
[21] Jayant S. Sabnis,et al. Calculation of particle trajectories in solid-rocket motors with arbitrary acceleration , 1992 .
[22] I. D. Parsons,et al. COUPLED FLUID-STRUCTURE 3-D SOLID ROCKET MOTOR SIMULATIONS , 2001 .
[23] R. S. Brown,et al. Internal flow field studies in a simulated cylindrical port rocket chamber , 1990 .
[24] R. S. Brown,et al. Coupling between acoustic velocity oscillations and solid-propellantcombustion , 1986 .
[25] H. Seifert,et al. Rocket Propulsion Elements , 1963 .
[26] Gary A. Flandro,et al. Aeroacoustic Instability in Rockets , 2001 .
[27] Jean-Philippe Pineau,et al. Spatial instability of planar channel flow with fluid injection through porous walls , 1998 .
[28] Francois Vuillot,et al. 2D NAVIER-STOKES STABILITY COMPUTATIONS FOR SOLID ROCKET MOTORS : ROTATIONAL, COMBUSTION AND TWO-PHASE FLOW EFFECTS. , 1997 .