Study of thermal throat of RBCC combustor based on one-dimensional analysis

Roncioni, 2015, Numerical simulation and performance assessment of a scramjet powered cruise vehicle at Mach 8, Aerosp. Sci. Technol., 42, 218, 10.1016/j.ast.2015.01.006

Zhong, 2015, Effects of fuel cracking on combustion characteristics of a supersonic model combustor, Acta Astronaut., 110, 1, 10.1016/j.actaastro.2015.01.003

Donohue, 2014, Dual-mode scramjet flameholding operability measurements, J. Propul. Power, 30, 592, 10.2514/1.B35016

Wang, 2015, Experiment study on the effect of combustor configuration on the performance of dual-mode combustor, Aerosp. Sci. Technol., 42, 169, 10.1016/j.ast.2015.01.008

Sato, 2006, Development study of precooled-cycle hypersonic turbojet engine for flight demonstration, Acta Astronaut., 61, 367, 10.1016/j.actaastro.2007.01.012

Etele, 2014, Experiment investigation of an alternative rocket configuration for rocket-based combined cycle engines, J. Propul. Power, 30, 944, 10.2514/1.B35080

M. Bulman, A. Siebenhaar, The strutjet engine: exploding the myths surrounding high speed airbreathing propulsion, AIAA Paper 95-2475, 1995.

Hiraiwa, 2008, Recent progress in scramjet/combined cycle engines at JAXA, Kakuda space center, Acta Astronaut., 63, 565, 10.1016/j.actaastro.2008.04.011

C.F. Ehrlich, Early studies of RBCC applications and lessons learned for today, AIAA Paper 2000-3105, 2000.

A.P. Kothari, J.W. Livingston, C. Tarpley, et al., Rocket based combined cycle hypersonic vehicle for orbital access, AIAA Paper 2011-2338, 2011.

T. Fujikawa, T. Tsuchiya, S. Tomioka, Multi-objective, multidisciplinary design optimization of TSTO spanes with RBCC engines, AIAA Paper 2015-0650, 2015.

Brandt, 1969, One-dimensional combustor optimization, J. Spacecr. Rockets, 6, 570, 10.2514/3.29615

O’brien, 2001, Quasi-one-dimensional high-speed engine model with finite-rate chemistry, J. Propul. Power, 17, 1366, 10.2514/2.5889

Tian, 2014, Quasi-one-dimensional multimodes analysis for dual-mode scramjet, J. Propul. Power, 30, 1559, 10.2514/1.B35177

Heiser, 1994, 346

H. Ikawa, Rapid methodology for design and performance prediction of integrated scramjet/hypersonic vehicle, AlAA Paper 89-2682, 1989.

J.P. Drummond, Numerical investigation of the perpendicular injector flow field in a hydrogen fueled scramjet, AlAA Paper 79-1482, 1979.

H.H. Klein, P.C. Chan, A numerical investigation of scramjet combustor, AlAA Paper 89-2561, 1989.

Shapiro, 1953, 218

R.L. Daines, C.L. Merkle, Computational analysis of mixing and jet pumping in rocket ejector engines, AlAA Paper 95-2477, 1995.

Zhao, 1998, 134

Stoer, 1993, 434

Emanuel, 1986, 49