[1] Fuligno L., Micheli D., Poloni C., An integrated approach for optimal design of micro gas turbine combustors. Journal of Thermal Science, 2009, 18(2): 173–184.
[2] Lefebvre A.H., Ballal D.R., Gas turbine combustion: Alternative fuels and emissions. Taylor & Francis Group, 2010.
[3] Chong C.T., Lam S.S., Hochgreb S., Effect of mixture flow stratification on premixed flame structure and emissions under counter-rotating swirl burner configuration. Applied Thermal Engineering, 2016, 105: 905–912.
[4] Dhanuka S.K., Temme J.E., Driscoll J., Unsteady aspects of lean premixed prevaporized gas turbine combustors: flame-flame interactions. Journal of Propulsion and Power, 2011, 27(3): 631–641.
[5] Temme J.E., Allison P.M., Driscoll J.F., Combustion instability of a lean premixed prevaporized gas turbine combustor studied using phase-averaged PIV. Combustion and Flame, 2014, 161(4): 958–970.
[6] Wang B., Zhang C., Lin Y., et al., Influence of main swirler vane angle on the ignition performance of TELESS-II combustor. Journal of Engineering for Gas Turbines and Power, 2016, 139(1): 011501.
[7] Mi X., Zhang C., Wang B., et al., Influence of main stage air splits on the ignition performance of TELESS-II combustor. ASME Turbo Expo 2017: Turbomachinery Technical Conference and Exposition, Charlotte, US, GT2017-63216.
[8] Bishop K., Allan W., Effects of fuel nozzle condition on gas turbine combustion chamber exit temperature distributions. ASME Turbo Expo 2010: Power for Land, Sea, and Air, Glasgow, UK, GT2010-23441.
[9] Karagozian A.R., Transverse jets and their control. Progress in Energy and Combustion Science, 2010, 36(5): 531–553.
[10] Walker R.E., Kors D.L., Multiple jet study. NASA-CR-121217, 1973.
[11] Srinivasan R., Berenfeld A., Mongia H.C., Dilution jet mixing program, phase 1. NASA-CR-168031, 1982.
[12] Srinivasan R., Berenfeld A., Mongia H.C., Dilution jet mixing program, phase 2. NASA CR-174624, 1982.
[13] Vranos A., Liscinsky D., True B., et al., Experimental study of cross-stream mixing in a cylindrical duct. 27th Joint Propulsion Conference, Sacramento, US, AIAA1991-2459.
[14] Oechsle V., Mongia H., Holdeman J., An analytical study of dilution jet mixing in a cylindrical duct. 29th Joint Propulsion Conference and Exhibit, Monterey, US, AIAA1993-2043.
[15] Liscinsky D., True B., Vranos A., et al., Experimental study of cross-stream mixing in a rectangular duct. 28th Joint Propulsion Conference and Exhibit, Nashville, US, AIAA1992-3090.
[16] Liscinsky D., True B., Holdeman J., Experimental investigation of crossflow jet mixing in a rectangular duct. 29th Joint Propulsion Conference and Exhibit, Monterey, US, AIAA1993-2037.
[17] Kroll J., Sowa W., Samuelsen G., et al., Optimization of circular orifice jets mixing into a heated crossflow in a cylindrical duct. 31st Aerospace Sciences Meeting, Reno, US, AIAA1993-249.
[18] Holdeman J., Srinivasan R., Coleman E., et al., Experiments in dilution jet mixing—Effects of multiple rows and non-circular orifices. 21st Joint Propulsion Conference, Monterey, US, AIAA1985-1104.
[19] Holdeman J., Srinivasan R., Berenfeld A., Experiments in dilution jet mixing. 19th Joint Propulsion Conference, Seattle, US, AIAA1983-1201.
[20] Holdeman J., Srinivasan R., Perspectives on dilution jet mixing. 22nd Joint Propulsion Conference, Huntsville, US, AIAA86-1611.
[21] Holdeman J., Perspectives on the mixing of a row of jets with a confined crossflow. 19th Joint Propulsion Conference, Seattle, US, AIAA1983-1200.
[22] Hatch M., Sowa W., Samuelson G., et al., Jet mixing into a heated cross flow in a cylindrical duct—Influence of geometry and flow variations. 30th Aerospace Sciences Meeting and Exhibit, Reno, US, AIAA1992-773.
[23] Holdeman J.D., Smith T.D., Clisset J.R., et al., A spreadsheet for the mixing of a row of jet with a confined crossflow. NASA/TM—2005-213137, 2005.
[24] Holdeman J.D., Clisset J.R., Moder J.P., Spreadsheet calculations of jets in crossflow: opposed rows of inline and staggered round holes. Heat and Mass Transfer, 2012, 48(2): 413–424.
[25] Bazdidi-Tehrani F., Teymoori A., Ghiyasi M., Sensitivity analysis of pollutants and pattern factor in a gas turbine model combustor due to changes in stabilizing jets characteristics. Journal of Thermal Science, 2022, 31(5): 1622–1641.
[26] Wang W., Yang S., Gao C., et al., Influence of turbulence schmidt number on exit temperature distribution of an annular gas turbine combustor using flamelet generated manifold. Journal of Thermal Science, 2020, 29(1): 58–68.
[27] Lu H., Liu F., Wang Y., et al., The effect of different reaction mechanisms on combustion simulation of a reverse-flow combustor. Journal of Thermal Science, 2020, 29(3): 793–812.
[28] Vignat G., Durox D., Candel S., The suitability of different swirl number definitions for describing swirl flows: Accurate, common and (over-) simplified formulations. Progress in Energy and Combustion Science, 2022, 89: 100969.
