Prediction of 3D Boundary Layer Blockage and the Grain Design Optimization of HVT Dual-thrust Hybrid Rockets

[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.