Experimental and numerical analysis of circular pulse jets

Journal of Fluid Mechanics

Volumn 392, Issue , 1999, Pages 129-153

  Ishii, R ^a   Fujimoto, H ^a   Hatta, N ^a   Umeda, Y ^b  

^a KYOTO UNIVERSITY   (Japan)

^b KYOTO UNIVERSITY   (Japan)

Author keywords

[No Author keywords available]

Indexed keywords

FLOW INTERACTIONS; MATHEMATICAL MODELS; SUPERSONIC FLOW; UNSTEADY FLOW;

CIRCULAR PULSE JETS; EULER EQUATIONS;

JETS;

EID: 0032626742     PISSN: 00221120     EISSN: None     Source Type: Journal    
DOI: 10.1017/S0022112099005303     Document Type: Article

References (19)

1. ABE, A. & TAKAYAMA, K. 1990 Numerical simulation and density measurement of a shock wave discharge from the open end of a shock tube. JSME Intl J. II 33, 246-223.
2. ADDY, A. L. 1981 Effect of axisymmetric sonic nozzle geometry on Mach disk characteristics. AIAA J. 19, 121-122.
3. CHAKRAVARTHY, S. R. & OSHER, S. 1985 A new class of high accuracy TVD schemes for hyperbolic conservation laws. AIAA Paper 85-0363.
4. ELDER, F. K. JR. & DE HAAS, N. 1952 Experimental study of the formation of a vortex ring at the open end of a cylindrical shock tube. J. Appl. Phys. 23, 1065-1069.
5. GOLUB, V. V. 1994 Development of shock wave and vortex structures in unsteady jets. Shock Waves 3, 279-285.
6. KUHL, A. L., REINHENBACH, H., NEUWALD, P., FERGUSON, R. E. & OPPENHEIM, A. K. 1997 Fluid mechanics of a planar exothermic jet. JSME ICFE-97, pp. 955-959.
7. MATSUDA, T., UMEDA, Y., ISHII, R., YASUDA, A. & SAWADA, K. 1987 Numerical and experimental studies on choked underexpanded jets. AIAA Paper 87-1378.
8. OPPENHEIM, A. K. & MAXON, J. A. 1991 Thermodynamics of combusion in an enclosure, dynamics of heterogeneous combustion and reacting system. Progress in Astronautics and Aeronautics, vol. 1 (ed. A. L. Kuhl, J. G. Leyer, A. A. Borisov & W. A. Sirignano) pp. 251-261. AIAA.
9. PANDA, J. 1998 Shock oscillation in underexpanded screeching jets. J. Fluid Mech. 363, 173-198.
10. PAYMAN, W. & SHEPHERD, W. C. F. 1946 Explosion and shock waves VI. The disturbance produced by bursting diaphragm with compressed air. Proc. R. Soc. Lond. A 186, 293-321.
11. POWELL, A., UMEDA, Y. & ISHII, R. 1992 Observation of the oscillation modes of circular choked jets. J. Acoust. Soc. Am. 92, 2823-2836.
12. RAMAN, G. 1998 Advances in underexpanding supersonic jet screech. AIAA Paper 98-0279.
13. SCHMIDT, E. M. & SHEAR, D. D. 1975 Optical measurements of muzzle blast. AIAA J. 13, 1086-1091.
14. SKEWS, B. W. 1966 The shape of a diffraction of shock wave. J. Fluid Mech. 29, 297-304.
15. SKEWS, B. W. 1967 The perturbed region behind a diffracting shock wave. J. Fluid Mech. 29, 705-720.
16. TAKAYAMA, K. & SEKIGUCHI, H. 1981 Formation and diffraction of spherical shock waves in a shock tube. Rep. Inst. High Speed Mech., Tohoku Univ., vol. 43, pp. 89-119.
17. UMEDA, Y. & ISHII, R. 1993 Oscillation modes of underexpanded jets issuing from square and equilateral triangular nozzles. J. Acoust. Soc. Am. 95, 1853-1857.
18. UMEDA, Y, MAEDA, H. & ISHII, R. 1987 Discrete tones generated by the impingement of a high-speed jet on a circular cylinder. Phys. Fluids 30, 2380-2388.
19. YANG, J. M. & TAKAYAMA, K. 1997 Shock wave diffraction at a 90° convex corner-A Report of Recent Development. JSME ICFE-97, pp. 157-161.