共 50 条
- [41] One-dimensional dynamic model of combustion process in the ABE chamber. Part 1 IZVESTIYA VYSSHIKH UCHEBNYKH ZAVEDENII AVIATSIONAYA TEKHNIKA, 1999, (03): : 59 - 63
- [42] One-dimensional dynamic model of combustion process in the ABE chamber. Part II IZVESTIYA VYSSHIKH UCHEBNYKH ZAVEDENII AVIATSIONAYA TEKHNIKA, 2000, (02): : 48 - 50
- [43] 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
- [44] Measurement of Fuel Concentration in the Vicinity of the Combustion Chamber Surface by Infrared Laser Absorption Method JOURNAL OF THERMAL SCIENCE AND TECHNOLOGY, 2010, 5 (02): : 282 - 292
- [46] STUDY OF COMBUSTION STABILITY IN A SWIRLING FLOW COMBUSTION CHAMBER RECHERCHE AEROSPATIALE, 1974, (01): : 37 - 48
- [48] Modeling of internal two-phase flow field inside a turbojet combustion chamber. Application to in-flight re-light Khimicheskaya Fizika, 2004, 23 (09): : 28 - 37
- [49] Pulsating combustion of gas fuel in the combustion chamber with closed resonant circuit LOW TEMPERATURE PLASMA IN THE PROCESSES OF FUNCTIONAL COATING PREPARATION, 2013, 479