共 11 条
- [1] Mathematical Model of Turbojet Engine Combustion Chamber Primary Zone FME TRANSACTIONS, 2007, 35 (01): : 29 - 34
- [2] DUAL FREQUENCY BAND THEORY OF UNSTABLE TURBULENT COMBUSTION OSCILLATIONS IN ROCKET ENGINE CHAMBER. Soviet Aeronautics (English translation of Izvestiya VUZ, Aviatsionnaya Tekhnika), 1977, 20 (03): : 10 - 14
- [3] Optical diagnostics and instrumentation for supercritical combustion studies in a LOX/H2 rocket engine combustion chamber ICIASF'03 RECORD: 20TH INTERNATIONAL CONGRESS ON INSTRUMENTATION IN AEROSPACE SIMULATION FACILITIES, 2003, : 296 - 303
- [4] Effect of distributed injection of air into the afterburning chamber of a ram-rocket engine on the efficiency of combustion of boron particles Combustion, Explosion, and Shock Waves, 2017, 53 : 652 - 664
- [6] Flow field and species concentration measurements in the primary zone of an aero-engine combustion chamber ADVANCES IN MECHANICAL ENGINEERING, 2018, 10 (01):
- [7] INVESTIGATION OF HEAT IRRADIATION AT A PRIMARY ZONE OF THE GAS-TURBINE ENGINE COMBUSTION-CHAMBER IZVESTIYA VYSSHIKH UCHEBNYKH ZAVEDENII AVIATSIONAYA TEKHNIKA, 1986, 3 : 82 - 84
- [8] Effect of air-inlet structures on combustion and flow field of inner wall in secondary combustion chamber of solid rocket ramjet Beijing Hangkong Hangtian Daxue Xuebao/Journal of Beijing University of Aeronautics and Astronautics, 2019, 45 (05): : 989 - 998
- [10] SIMULATION OF CO EMISSION IN PRIMARY AND SECONDARY ZONE OF A SMALL GAS TURBINE COMBUSTION CHAMBER USING CFD AND REACTORS NETWORK PROCEEDINGS OF THE ASME GAS TURBINE INDIA CONFERENCE, 2019, VOL 2, 2020,