Study on breakup of conical liquid sheet under varying flow conditions

Chinese Journal of Aeronautics

Volumn 16, Issue 1, 2003, Pages 12-14

  Yue, Ming ^a   Xu, Hang ^a   Yang, Mao Lin ^a   Yuan, Hui Jin ^b   Sheng, Shen Zhi ^b  

^a BEIHANG UNIVERSITY   (China)

^b PEKING UNIVERSITY   (China)

Author keywords

Breakup of conical liquid sheet; Disturbance wave; PIV; Pressure swirl atomizer

Indexed keywords

ATOMIZATION; ATOMIZERS; CAMERAS; CHARGE COUPLED DEVICES; DROP BREAKUP; LASER BEAMS; NOZZLES; PRESSURE MEASUREMENT; VELOCITY MEASUREMENT;

CONICAL LIQUID SHEET; DISTURBANCE WAVE; PARTICLE IMAGE VELOCIMETRY; PRESSURE SWIRL ATOMIZER;

AERODYNAMICS;

EID: 1842627857     PISSN: 10009361     EISSN: None     Source Type: Journal    
DOI: 10.1016/S1000-9361(11)60164-7     Document Type: Article

References (6)

1. Feikema D A. Liquid film characteristics inside a pressure-swirl atomizer[R]. AIAA Paper 98-3692, 1998.
2. Holtzclaw D, Sakman T, Jeng S M, et al. Investigation of flow in a simplex fuel nozzle[R]. AIAA Paper 97-2970, 1997.
3. Hirt C W, Amsden A A, Cook J L. An arbitrary Lagrangian-Eulerian computing method for all flow speeds[J]. J Computational Physics, 1974, 14, 227-253.
4. Sakman A T, Jog M A, Jeng S M, et al. Parametric study of simplex fuel nozzle internal flow and performance[R]. AIAA 98-3906, 1998.
5. Jeng S M, Jog M A, Benjamin M A. Computational and experimental study of liquid sheet emanating from simplex fuel nozzle[R]. AIAA 97-0796, 1997.
6. Lefebvre A H. Gas turbine combustion[M]. McGraw-Hill Book Company, 1983.