Numerical and experimental analysis of heat transfer in injector plate of hydrogen peroxide hybrid rocket motor

Acta Astronautica - Tập 128 - Trang 286-294 - 2016
Guobiao Cai1, Chengen Li1, Hui Tian1
1School of Astronautics, Beihang University, Beijing 100191, China

Tóm tắt

Từ khóa


Tài liệu tham khảo

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

Galfetti, 2014, An Italian network to improve hybrid rocket performance, Acta Astronaut., 96, 246, 10.1016/j.actaastro.2013.11.036

Casalino, 2014, Optimization of hybrid upper-stage motor with coupled evolutionary/indirect procedure, J. Propul. Power, 30, 1390, 10.2514/1.B35111

Amri, 2013, The design, development and test of one newton hydrogen peroxide monopropellant thruster, Aerosp. Sci. Technol., 25, 266, 10.1016/j.ast.2012.02.002

Adachi, 2015, Liquid films instability analysis of liquefying hybrid rocket fuels under supercritical conditions, AIAA J., 53, 1578, 10.2514/1.J053459

Li, 2016, Numerical analysis of combustion characteristics of hybrid rocket motor with multi-section swirl injection, Acta Astronaut., 123, 26, 10.1016/j.actaastro.2016.02.023

Zhu, 2013, Injector head transpiration cooling coupled with combustion in H2/O2 subscale thrust chamber, J. Thermophys. Heat. Transf., 27, 42, 10.2514/1.T3872

Jang, 2015, Design and validation of a liquid film-cooled hydrogen peroxide/kerosene bipropellant thruster, J. Propul. Power, 31, 761, 10.2514/1.B35434

Natali, 2016, Ablation modeling of state of the art EPDM based elastomeric heat shielding materials for solid rocket motors, Comp. Mater. Sci., 111, 460, 10.1016/j.commatsci.2015.09.050

Davydenko, 2007, Hybrid rocket engines, Aerosp. Sci. Technol., 11, 55, 10.1016/j.ast.2006.08.008

Daniel, 2011, Design and analysis of a reusable N2O-cooled aerospike nozzle for labscale hybrid rocket motor testing, AIAA Pap., 2011

Zhao, 2015, Steady-state coupled analysis of flowfields and thermochemical erosion of C/C nozzles in hybrid rocket motors, Sci. China Technol. Sci., 58, 574, 10.1007/s11431-015-5775-6

Tobias, 2015, Failure mode investigation of a sorbitol-based hybrid rocket flight motor for the Stratos II sounding rocket, AIAA Pap., 2015

Li, 2014, Experimental investigation of fuel regression rate in a HTPB based lab-scale hybrid rocket motor, Acta Astronaut., 105, 95, 10.1016/j.actaastro.2014.08.028

P. Zeng, X. Li, J. Li, Development of the Variable Thrust Hybrid Sounding Rocket: Beihang-3, Paper IAC-12-E2.3.5, 2012.

Barato, 2015, Numerical model to analyze transient behavior and instabilities on hybrid rocket motors, J. Propul. Power, 31, 643, 10.2514/1.B35282

Tian, 2014, Numerical and experimental studies of the hybrid rocket motor with multi-port fuel grain, Acta Astronaut., 96, 261, 10.1016/j.actaastro.2013.12.001

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

Barik, 2015, Heat transfer enhancement from a small rectangular channel with different surface protrusions by a turbulent cross flow jet, Int. J. Therm. Sci., 98, 32, 10.1016/j.ijthermalsci.2015.07.003

Li, 2013, Three-dimensional numerical simulation of two-phase flow in hybrid rocket motor, AIAA Pap., 2013

Tyurenkova, 2012, Non-equilibrium diffusion combustion of a fuel droplet, Acta Astronaut., 75, 78, 10.1016/j.actaastro.2012.01.010

Dushin, 2008, Mathematical simulation for non-equilibrium droplet evaporation, Acta Astronaut., 63, 1360, 10.1016/j.actaastro.2008.05.021

Smirnov, 1996, Unsteady state evaporation in weightlessness, Acta Astronaut., 39, 561, 10.1016/S0094-5765(96)00162-2

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

Tian, 2014, Transient simulation of regression rate on thrust regulation process in hybrid rocket motor, Chin. J. Aeronaut., 27, 1343, 10.1016/j.cja.2014.08.016

Tian, 2013, Numerical and experimental investigation on the effects of aft mixing chamber diaphragm in hybrid rocket motor, Sci. China Technol. Sci., 56, 2721, 10.1007/s11431-013-5325-z

Tyurenkova, 2016, Material combustion in oxidant flows, Acta Astronaut., 120, 129, 10.1016/j.actaastro.2015.11.033

Smirnov, 2015, Laminar diffusion flame propagation over thermally destructing material, Acta Astronaut., 109, 217, 10.1016/j.actaastro.2014.09.016

Smirnov, 2015, Accumulation of errors in numerical simulations of chemically reacting gas dynamics, Acta Astronaut., 117, 338, 10.1016/j.actaastro.2015.08.013

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

D.D. Davis, L.A. Dee, B. Greene, S.D. Hornung, M.B. McClure, K.A. Rathgeber, Fire, Explosion, Compatibility and Safety Hazards of Hydrogen Peroxide, NASA Technical Memorandum TM-2004-213151, NASA Johson Space Center White Sand Test Facility, 2005.

Ricciardi, 1981, A simplified method to predict the charred thickness of the thermal insulation in solid rocket motors, AIAA Pap., 81