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Page | 014 3.2.1.4.2 Low Swirl Combustion
3.2.1.4.2-8 Notes
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1. C.K. Chan et al., “Freely Propagating Open Premixed Turbulent Flames Stabilized by Swirl,”Proc. Comb. Inst., 24 (1992): 511-
518; B. Bedat and R.K. Cheng, “Experimental Study of Premixed Flames in Intense Isotropic Turbulence,” Combustion and
Flame 100, no. 3 (1995): 485-494; R.K. Cheng, “Velocity and Scalar Characteristics of Premixed Turbulent Flames Stabilized
By Weak Swirl,” Combustion and Flame 101, no.1-2 (1995): 1-14.
2. R.K.Cheng, 1998. Ultralean Low Swirl Burner. U.S. Patent 5735681, (The Regents of the University of California), fi led
March 19, 1993 and issued April 7, 1998; R.K. Cheng and D.T. Yegian, 1999. Mechanical Swirler for a Low-NOx
Weak-
Swirl Burner. U.S. Patent 5,879,148, (The Regents of the University of California), fi led April 16, 1997 and issued March 9,
1999 .
3. N. Syred and J.M. Beer, “Combustion in Swirling Flow: A Review,” Combustion and Flame 23 (1974): 143-201.
4. T. Plessing et al., “Measurement of the Turbulent Burning Velocity and the Structure of Premixed Flames on a Low Swirl
Burner,” Proc. Comb. Inst. 28 (2000): 359-366; I. G. Shepherd et al., “Premixed Flame Front Structure in Intense Turbulence,”
Proc. Comb. Inst. 29 (2002): 1833-1840; R.K. Cheng, et al., “Premixed Turbulent Flame Structures in Moderate and
Intense Isotropic Turbulence,” Combustion Science and Technology 174, no.1(2002): 29-59; C. Kortschik, T. Plessing, and N.
Peters, “Laser Optical Investigation of Turbulent Transport of Temperature Ahead of the Preheat Zone in a Premixed Flame,”
Combustion and Flame 136, no.1-2 (2004): 43-50; L.P.H. de Goey et al., “Analysis of the Flame Thickness of Turbulent
Flamelets in the Thin Reaction Zones Regime,” Proc. Comb. Inst. 30, no 1 (2005): . 859-866; also see
note 2 above.
5. See note 2 above (Bedat & Cheng).
6. See note 1 above.
7. See note 2 above (Bedat & Cheng).
8. See note 4 above.
9. M.R. Johnson et al., “A Comparison of the Flowfi elds and Emissions of High-swirl Injectors and Low-swirl Injectors for
Lean Premixed Gas Turbines,” Proc. Comb. Inst. 30 (2005): 2867 - 287
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