Computational and Experimental Investigation of Supersonic Flow and their Controls
Autor: | Vasana M. Don, Avital, Eldad J., Fariborz Motallebi |
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Jazyk: | angličtina |
Rok vydání: | 2013 |
Předmět: | |
DOI: | 10.5281/zenodo.1076048 |
Popis: | Supersonic open and closed cavity flows are investigated experimentally and computationally. Free stream Mach number of two is set. Schlieren imaging is used to visualise the flow behaviour showing stark differences between open and closed. Computational Fluid Dynamics (CFD) is used to simulate open cavity of flow with aspect ratio of 4. A rear wall treatment is implemented in order to pursue a simple passive control approach. Good qualitative agreement is achieved between the experimental flow visualisation and the CFD in terms of the expansion-shock waves system. The cavity oscillations are shown to be dominated by the first and third Rossister modes combining to high fluctuations of non-linear nature above the cavity rear edge. A simple rear wall treatment in terms of a hole shows mixed effect on the flow oscillations, RMS contours, and time history density fluctuations are given and analysed. {"references":["Krishnamurty, K., ÔÇÿAcoustic radiation from two-dimensional rectangular\ncutouts in aerodynamic surfaces-, National Advisory Committee for\nAeronautics (N.A.C.A.) Technical Note 3487, 1955.","Tam, C. K. W. and Block, P. J. W., ÔÇÿOn the Tones and Pressure\nOscillations Induced by Flow over Rectangular Cavities-, Journal of\nFluid Mechanics, 89: 373-99, 1978.","Rockwell, D. and Naudascher, E., ÔÇÿSelf-Sustained Oscillations of\nImpinging Free Shear Layers-, Annual Review of Fluid Mechanics, 11:\n67-94, 1979.","Dellprat, N., ÔÇÿRossiters formula- A simple spectral model for a complex\namplitude modulation process?-, Physics of Fluids, 18, 7, 2006.","Tracy, M. B., Plentovich, E. B., Chu, J. and Langley Research Centre,\nÔÇÿMeasurements of fluctuating pressure in a rectangular cavity in\ntransonic flow at High Reynolds numbers-, National Aeronautics and\nSpace Administration (NASA) Technical Memorandum 4363, 1992","Suponitsky, V., Avital, E. and Gaster, M., ÔÇÿOn three-dimensionality and\ncontrol of incompressible cavity flow-, Physics of Fluid, 17, 104103,\n2005.","Rowley, C. W., Colonius, T. and Basu, A. J., ÔÇÿOn self-sustained\noscillations in two-dimensional compressible flow over rectangular\ncavities. Journal of Fluid Mechanics, 455: 315-346, 2002.","Heller, H. H. And Bliss, D. B., ÔÇÿAerodynamically Induced Pressure\nOscillations in Cavities - Physical Mechanisms and Suppression\nConcepts-, Air Force Flight Dynamics Laboratory Technical Report\nAFFDL-TR-74-133, 1975.","William, D. R., Cornelius, D. and Rowley, C. W., ÔÇÿSupersonic Cavity\nResponse to Open-Loop Forcing-, Active Flow Control, 95: 230-43,\n2007.\n[10] Mohri, K. & Hiller, R. Computational and experimental study of\nsupersonic flow over axisymmetric cavities. Shock Waves, 21, 175-191,\n2011.\n[11] Delprat, N., ÔÇÿRossiter-s formula: A simple spectral model for a complex\namplitude modulation process?-, Fluids of Physics, 18, 2006.\n[12] Williams, D. R. and Rowley, C. W., ÔÇÿRecent Progress in Closed-Loop\nControl of Cavity Tones-, AIAA paper 2006-0712, 44th Aerospace\nSciences Meeting and Exhibit, Reno, Nevada, USA, 2006.\n[13] Punekar J., Avital EJ and Musafir RE, Computations of Nonlinear\nPropagation of Sound Emitted from High Speed Mixing Layers, Open\nAcoustics Journal 3, 11-20, 2010.\n[14] Hirsch C, Numerical computation of internal and external flows, vol. 2,\nComputational methods for inviscid and viscous flows, 1John Wiley &\nSons 1992.\n[15] Avital EJ, Musafir RE and Korakianitis T, Nonlinear Propagation of\nSound Emitted by High Speed Wave Packets, Journal of Computational.\nAcoustics in press."]} |
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