Planar laser imaging of a supersonic side-facing cavity

37th Aerospace Sciences Meeting and Exhibit

Volumn , Issue , 1999, Pages

  Unalmis O H ^a   Clemens, N T ^a   Dolling, D S ^a  

^a The University of Texas at Austin   (United States)

Author keywords

[No Author keywords available]

Indexed keywords

AEROSPACE ENGINEERING; COHERENT SCATTERING; PRESSURE MEASUREMENT; WALL FLOW;

CAVITY ACOUSTICS; COHERENT STRUCTURE; CONDITIONAL AVERAGE; ENSEMBLE AVERAGES; FLUCTUATING PRESSURES; OSCILLATION CYCLES; RECTANGULAR CAVITY; TURBULENT STRUCTURES;

SHEAR FLOW;

EID: 84983177578     PISSN: None     EISSN: None     Source Type: Conference Proceeding    
DOI: None     Document Type: Conference Paper

References (19)

1. Rossiter, J. E., “Wind-Tunnel Experiments on the Flow Over Rectangular Cavities at Subsonic and Transonic Speeds,” A.R.C.R. & M., No. 3438, 1966.
2. Maurer, O. F., “Investigation and Reduction of Open Weapon Bay Pressure Oscillations Expected in the B-1 Aircraft,” AFFDLTM 74-101, 1973.
3. Rockwell, D., and Naudascher, E., “Review-Self-Sustaining Oscillations of Flow Past Cavities,” ASME J. FluidEngr., Vol. 100, 1978, pp. 152-165.
4. Stallings, Jr. R. L., “Store Separation from Cavities at Supersonic Flight Speeds,” Spacecraft, Vol. 20, 1983, pp. 129-132.
5. Zhang, X., and Edwards, J. A., “An Investigation of Supersonic Oscillatory Cavity Flows Driven by Thick Shear Layers,” Aeronautical Journal 1990, pp. 355-364.
6. Rizzetta, D. P., “Numerical Simulation of Supersonic Flow Over a Three-Dimensional Cavity,” AIAA, Journal, Vol. 26, 1988, pp. 799-807.
7. Perng, S. ft., and Dolling, D. S., “Passive Control of Pressure Ösciliaüqns in Hypersonic Cavity Flow,” AIAA Paper 96-0444, Jan. 1996.
8. Pereira, J. Ç. F., and Sousa, J. M. M., “Experimental and Numerical Investigation of Flow Oscillations in a Rectangular Cavity,” ASMEJ. Fluid Engr., Vol. 117, 1995, pp. 68-74.
9. Morgenstern, Jr. A., and Chokani, N., “Hypersonic Flow Past Open Cavities,” AÎÀA Paper 93-2969, 1993.
10. Heller, H. H., and Bliss, D. B., “The Physical Mechaiiism of Flow-Induced Pressure Fluctuations in Cavities and Concepts for Their Suppression,” AIAA Paper 75-491, 1975.
11. Heller, H.j H., Holmes, G., and Covert, E. E., “Flow-Induced Pressure Oscillations in Shallow Cavities,” AFFDL-TR-70-104, Dec. 1970.
12. l2 Ünalmis, p. H., Clemens, N. T., and Dolling, D. S., “Planar Laser Imaging of High Speed Cavity Flow Dynamics,” AIAA Paper 98-0776, Jan. 1998.
13. Chan, S. C, Clemens, N. T., and Dolling, D. S., “Flow field Imaging of Unsteady, Separated Compression Ramp Interactions,” AIAA Paper 95-2195, Jjune 1995.
14. Murray, R. C, and Elliott, G. S., “The Compressible Shear Layer Over a Two-Dimensional Cavity,” AIAA Paper 98-0430, Jan. 1998
15. Beresh S.J, Cpmninos, M., Clemens, T., and Dolling, D. S., “The Effects of Incoming Turbulent Boundary Layer Structure on a Shock Induced Separated Flow,” AIAA Paper 98-Ö62Ö, Jan. 1998.
16. Beresh, S. J., “The Effects of the Incoming Turbulent Boundary Layer on a Shock-Induced Separated Flow using Particle Image Velocimetry,” Ph.D. Dissertation, Dept. of Aerospace Engineering and Engineering Mechanics, The University of Texas at Austin, to be defended in May 1999.
17. l7 Rehm, J. E., “The Effects of Heat Release on Planar Jet Diffusion Flames,” Ph.D. Dissertation, Dept. of Aerospace Engineering and Engineering Mechanics, The University of Texas at Austin, December 1998.
18. Cattafesta, L. N., Garg, S., Kegerise, M. S.T and Jones, G. S., “Experiments on Compressible Flow-Induced Cavity Oscillations,” AIAA Paper 98-2912, June 1998.
19. Clemens, N. T., and Mungal, M. G., “Two- and Three-Dimensional Effects in the Supersonic Mixing Layer,” AIAA Journal, Vol. 30, No. 4, 1992, pp. 973-981.