Numerical investigations of hybrid rocket engines

Barato, 2016, Integrated approach for hybrid rocket technology development, Acta Astronaut., 128, 257, 10.1016/j.actaastro.2016.07.023

Cai, 2017, Transient analysis on ignition process of catalytic hybrid rocket motor, Aero. Sci. Technol., 67, 366, 10.1016/j.ast.2017.03.041

Tian, 2017, Three-dimensional numerical and experimental studies on transient ignition of hybrid rocket motor, Acta Astronaut., 140, 247, 10.1016/j.actaastro.2017.08.022

Chiba, 2016, Extinction–reignition superiority in a single-stage sounding hybrid rocket, Aero. Sci. Technol., 58, 437, 10.1016/j.ast.2016.09.010

Sun, 2016, Regression rate behaviors of HTPB-based propellant combinations for hybrid rocket motor, Acta Astronaut., 119, 137, 10.1016/j.actaastro.2015.11.015

Chidambaram, 2015, A numerical investigation of oxidizer mixed hybrid rocket motors, Aero. Sci. Technol., 45, 10, 10.1016/j.ast.2015.04.005

Lestrade, 2015, Liquefying fuel regression rate modeling in hybrid propulsion, Aero. Sci. Technol., 42, 80, 10.1016/j.ast.2014.11.015

Gariani, 2011, Numerical simulation of HTPB combustion in a 2D hybrid slab combustor, Acta Astronaut., 69, 289, 10.1016/j.actaastro.2011.03.015

Pei, 2014, Numerical investigation on cavity structure of solid-fuel scramjet combustor, Acta Astronaut., 105, 463, 10.1016/j.actaastro.2014.09.009

Ben-Yakar, 1998, Investigation of a solid fuel scramjet combustor, J. Propul. Power, 14, 447, 10.2514/2.5321

Sun, 2015, Regression rate and combustion performance investigation of aluminum metallized HTPB/98HP hybrid rocket motor with numerical simulation, Aero. Sci. Technol., 42, 287, 10.1016/j.ast.2015.01.014

Rybanin, 1988, Combustion wave propagation on a combustible material surface in a heterogeneous reaction, Combust. Explos. Shock Waves, 24, 416, 10.1007/BF00750012

Tyurenkova, 2016, Material combustion in oxidant flows: self-similar solutions, Acta Astronaut., 120, 129, 10.1016/j.actaastro.2015.11.033

Schlichting, 1979

Dorrance, 1962

Smirnov, 2017, Detonation onset following shock wave focusing, Acta Astronaut., 135, 114, 10.1016/j.actaastro.2016.09.014

Smirnov, 2014, Hydrogen fuel rocket engines simulation using LOGOS code, Int. J. Hydrogen Energy, 39, 10748, 10.1016/j.ijhydene.2014.04.150