예막 공기충돌형 분사기의 벤추리 덤프면 설계

목차 (Table of Contents)

• ABSTRACT
• 초록
• 1. 서론
• 2. 분사기 및 벤추리 설계
• 3. 실험 조건 및 방법
• 4. 실험 결과
• 5. 결론
• References

참고문헌 (Reference)

1 Dhanuka, S. K., "Unsteady Aspects of Lean Premixed Prevaporized Gas Turbine Combustors : Flame-Flame Interactions" 27 (27): 631-641, 2011

2 Rizkalla, A. A., "The Influence of Air and Liquid Properties on Airblast Atomization" 97 (97): 316-320, 1975

3 Lefebvre, A. H., "The Development of an Air Blast Atomizer for Gas Turbine Application" 1966

4 Batarseh, F.Z.M., "Spray Generated by an Airblast Atomizer: Atomization, Propagation and Aerodynamics Instability" Technische Universität 2009

5 Choi, M. H., "Spray Characteristics of Jet According to Position of Injector Hole in Crossflow" 905-911, 2017

6 Yamamoto, T., "Research and Development of Staging Fuel Nozzle for Aeroengine" 639-646, 2009

7 Choi, S. M., "Research and Development Trend of Gas Turbine Combustor in Korea" 287-289, 2012

8 Gepperth, S., "Pre-filming primary atomization : Experiments and modeling" 2010

9 Im, K. S., "Parametric study of the swirler/ venturi spray injectors" 17 (17): 717-727, 2001

10 Lee, C. M., "NASA Project Develops Next Generation Low-Emissions Combustor Technologies" AIAA 2013

11 Francis, R. N. A., "Investigation of Fuel Nozzle Technologies to Reduce Gas Turbine Emissions" Toronto University 2015

12 Lefebvre, A.H., "Gas Turbine Combustion:Alternative Fuels and Emissions" CRC press 2010

13 Oberleithner, K., "Formation and Flame-Induced Suppression of the Precessing Vortex Core in a Swirl Combustor : Experiments and Linear Stability Analysis" 162 (162): 3100-3114, 2015

14 Matsuura, K., "Effects of Ambient Pressure on Sprays Characteristics a High Shear Type Aero-Engine Airblast Fuel Injector" 2008

15 Ercegovic, D. B., "Effect of Swirler-Mounted Mixing Venturi on Emissions of Flame-Tube Combustor Using Jet A Fuel" NASA 1979

16 Foust, M. J, "Development of the GE Aviation Low Emissions TAPS Combustor for Next Generation Aircraft Engines" AIAA 2012

17 Lazik, W., "Development of Lean-Burn Low-NOx Combustion Technology at Rolls-Royce Deutschland" 797-807, 2008

18 Yamamoto, T., "Combustion Characteristics of Fuel Staged Combustor for Aeroengines at LTO Cycle Conditions" 951-958, 2011

19 Jung, S. C., "CFD Simulation of a Prefilming Air Blast Fuel Nozzle" 251-253, 2017

20 Jasuja, A. K., "Behaviour of Aero-Engine Airblast Sprays in Practical Environment" 2006

21 Sun, H., "Atomization and Vaporization Characteristics of Airblast Fuel Injection Inside a Venturi Tube" 17-, 1993

22 Burkhalter, M. W., "Atomization and Mixing Performance of Swirl-Venturi Lean Direct Injection" Iowa University 2014

23 "Annual Report of the Council 2012"

24 Lefebvre, A. H., "An Improved Fuel Injection System for Gas Turbine Engines, US3283502"

25 Lefebvre, A. H., "Airblast Atomization" 6 (6): 233-261, 1980

26 Simmons, H. C., "Air-Atomizing Fuel Nozzle, US3980233"

27 Abernethy, R. B., "ASME Measurement Uncertainty" 107 (107): 161-164, 1985

28 Han, Y. M., "A Design of Low Emission Combustor for an Aero-Gas Turbine Engine with a Lean Fuel Module" 661-668, 2000