Prediction of 3D Boundary Layer Blockage and the Grain Design Optimization of HVT Dual-thrust Hybrid Rockets
暂无分享,去创建一个
N. Chandrasekaran | R. Baskaran | Pavithra Murugesh | V. S. Sanal Kumar | V. Sankar | Sulthan Ariff Rahman M
[1] N. Chandrasekaran,et al. Modeling of Sanal Flow Choking Condition and Design Optimization of High Performance Dual-thrust SRMs , 2018, 2018 Joint Propulsion Conference.
[2] Guobiao Cai,et al. Three-dimensional numerical and experimental studies on transient ignition of hybrid rocket motor , 2017 .
[3] Guobiao Cai,et al. Diameter and position effect determination of diaphragm on hybrid rocket motor , 2016 .
[4] V. R. Sanal Kumar,et al. Ignition Transient of Dual-Thrust Solid Propellant Rocket Motors - A Review , 2012 .
[5] M. Di Giacinto,et al. Internal Ballistics Simulation of a NAWC Tactical SRM , 2011 .
[6] Toshiaki Setoguchi,et al. Boundary-Layer Effects on Internal Flow Choking in Dual-Thrust Solid Rocket Motors , 2008 .
[7] Toshiaki Setoguchi,et al. Starting Transient Flow Phenomena in Inert Simulators of Solid Rocket Motors with Divergent Ports , 2006 .
[8] S. Raghunathan,et al. Fluid-Throat-Induced Shock Waves During the Ignition Transient of Solid Rockets , 2006 .
[9] J. Majdalani,et al. Higher Mean-Flow Approximation for Solid Rocket Motors with Radially Regressing Walls , 2002 .
[10] V. Yang,et al. Unsteady Flow Evolution in Porous Chamber with Surface Mass Injection, Part 1: Free Oscillation , 2001 .
[11] J. Majdalani. Boundary-Layer Structure in Cylindrical Rocket Motors , 1999 .
[12] R. W. Hermsen,et al. Flowfield in the Combustion Chamber of a Solid Propellant Rocket Motor , 1974 .
[13] H. Krier,et al. Analysis of the chemically reacting laminar boundary layer during hybrid combustion , 1973 .
[14] Fred E. C. Culick,et al. Rotational axisymmetric mean flow and damping of acoustic waves in asolid propellant rocket. , 1966 .
[15] G. Taylor. Fluid flow in regions bounded by porous surfaces , 1956, Proceedings of the Royal Society of London. Series A. Mathematical and Physical Sciences.