K. Krishnamurty, Acoustic Radiation from Two-Dimensional Rectangular Cutouts in Aerodynamic Surface, 1955, NACA TN-3487. | |
A. Roshko, Some Measurements of Flow in a Rectangular Cutout, 1955, NACA TN-3488. | |
J. E. Rossiter, Wind-Tunnel Experiments on the Flow over Rectangular Cavities at Subsonic and Transonic Speed, 1966, Report and Memoranda No. 3438. | |
H. H. Heller and D. Bliss, The Physical Mechanism of Flow-Induced Pressure Fluctuations in Cavities and Concepts of their Suppression, AIAA Paper, 1975, 491. | |
C. K. Tam and P. J. Block, On the Tones and Pressure Oscillations induced by Flow Over Rectangular Cavities, Journal of Fluid Mechanics, 1978, 89, 373-399. CrossRef | |
R. C. Bauer and R. E. Dix, Engineering Model of Unsteady Flow in a Cavity, 1991, AEDC-TR-91-17 | |
L. Cattefesta, D. Williams, C. Rowley, and F. Alvi, Review of active control flow induced cavity resonance, AIAA Paper, 2003, 3567. | |
L. N. Cattafesta, Q. Song, D. Willimas, C. W. Rowley, and F. S. Alvi, Active Control of Flow-Induced Cavity Oscillations, Progress in Aerospace Sciences, 2008, 44, 479-502. CrossRef | |
S. J. Moon, S. L. Gai, H. H. Kleine, and A. J. Neely, Supersonic Flow Over Straight Shallow Cavities In Leading and Trailing Edge Modification AIAA Paper, 2010, 4687. | |
R. C. Murray and G. S. Elliott, Characteristics of the Compressible Shear Layer over a Cavity, AIAA Journal, 2001, 39, 846-856. CrossRef | |
J. G. Dudley and L. Ukeiley, Suppression of Fluctuating Surface Pressure in a Supersonic Cavity Flow, AIAA Paper, 2010, 4974. | |
L. G. Kaufman and R. L. Clark, Mach 0.6 to 3.0 Flows Over Rectangular Cavities, 1983, AFWAL-TR-82-3112. | |
M. J. Stanek, G. Raman, V. Kibens, J. A. Ross, J. Odedra and J. W. Peto (200) Control of cavity resonance through very high frequency forcing, AIAA Paper, 2000, 1905. | |
R. F. Schmit and G, Ramen, High and low Frequency Actuation Comparison for a Weapons Bay Cavity, International Journal of Aeroaoustics, 2005, 5, 395. | |
R. F. Schmit, C. McGaha, J. Tekell, J. Grove, and M. Stanek, (2009) Performance Results for the Optical Turbulence Reduction Cavity, AIAA Paper, 2009, 702. | |
R. F. Schmit, F. Semmelmayer, M. Haverkamp, and J. Grove, Fourier Analysis of High Speed Shadowgraph Images around a Mach 1.5 Cavity Flow Field, AIAA Paper, 2011, 3961. | |
G. F. Clark, Trisonic Gasdynamic Facility User Manual, 1982, AFWAL-TM-82-176-FIMM. | |
J. P. Dussauge and A. J. Smits, Characteristic scales for energetic eddies in turbulent supersonic boundary layers, Experimental Thermal and Fluid Sciences, 1997, 14, 85-91. CrossRef | |
S. L. Birch, and J. M. Eggers, A critical review of experimental data for developed free turbulent shear layers, 1973, NASA SP321. | |
C. Pantano, and S. Sarkar, A study of compressibility effects in the high-speed turbulent shear layer using direct simulation, Journal of Fluid Mechanics, 2002, 14, 329-371. | |
N. T. Clemens and M. G. Mungal, Large-scale structures and entrainment in supersonic mixing layer, Journal of Fluid Mechanics, 1995, 248, 171-16. | |
G. M. Lilley, The generation of sound in turbulent motion, Aeronautical Journal, 2008, 112, 381-394. | |
W. Blumen, P. G. Dazing, D. F. Billings, Shear layer instability of inviscid compressible fluid, Journal of Fluid Mechanics, 1975, 71, 305-316. CrossRef | |
D. Papamoschou, and A. Roshko, The compressible turbulent shear layer: an experimental study, Journal of Fluid Mechanics., 1988, 197, 453-477. CrossRef | |
E. Schulein, and V. M. Trofimov, Steady longitudinal vortices in supersonic turbulent separated flows, Journal of Fluid Mechanics, 2011, 672, 451-476. CrossRef | |
M. J. Stanek, M. R. Visbal, D. P. Rizzetta, S. G. Rubin, and P. K. Khosla, On A Mechanism of Stabilizing Turbuelent Free Shear Layers in Cavity Flows, Computers & Fluids, 2007, 36, 1621-1637. CrossRef | |
X. Zhang, A. Rona, and J. A. Edwards, The effect of trailing edge geometry on cavity flow oscillations driven by a supersonic shear layer. Aeronautical Journal, 1998, 3, 129-136. | |
G. L. Bar, Experimental investigation of the sudden expansion of a supersonic plane flow into a 90oVee channel, 1972, MS Thesis, Aerospace Engineering Department, Wichita State University, KS. | |
A. Ahmed, and G. W. Zumwalt, Base Drag Reduction of a Non-Circular Missile, Journal of Spacecraft and Rockets, 1993, 30, 781-782. CrossRef | |
G. S. Settles, Schlieren and Shadowgraph Techniques: Visualizing Phenomena in Transparent Media, 2006 Springer, Berlin. | |
A. P. G. Peterson, E. E. Gross, Handbook of Noise Measurements. 1972, General Radio, Concord | |
J. E.F Williams, J. Simpson, and V. J. Virchis ‘Crackle’: an annoying component of jet noise, Journal of Fluid Mechanics, 1975, 75. | |
W. K. George, Lectures in Turbulence for the 21st Century, unpublished, 2011. | |
M. J. Stanek, J. A. Ross, J. Odegra, J. Peto, High Frequency Acoustic Suppression- The Mystery of the Rod-in-Crossflow Revealed, AIAA Paper, 2003, 0007. |
Examining Passive Flow Control using High Speed Shadowgraph Images in a Mach 1.5 Cavity Flow Field
Ryan SchmitRelated information
1 U.S Air Force Research Laboratory, 2130 Eight Street Wright-Patterson Air Force Base, OH 45433, USA
, James GroveRelated information1 U.S Air Force Research Laboratory, 2130 Eight Street Wright-Patterson Air Force Base, OH 45433, USA
, Anwar AhmedRelated information2 Auburn University, 211 Aerospace Engineering Bldg. Auburn, AL 36849-5338 USA