Abstract
A study is conducted on supersonic flow at Mach number 1.65 over rectangular cavity of length-to-depth (L/D) ratio 3. Schlieren visualization revealed normal shock train like pattern in flow over the cavity. These shock structure are unsteady, and oscillated longitudinally inside the test section over the cavity. The oscillating shock train is eliminated, as the blockage produced by shear layer and boundary layer thickening due to pressure recovery in cavity is reduced by offsetting the cavity aft wall. The shock train—shear layer coupling is observed to completely suppress the third and higher modes of cavity oscillations.
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References
Krishnamurthy, K.: Acoustic radiation from two-dimensional rectangular cutouts in aerodynamic surface. NASATN-3487 (1955)
Rossiter, J. E.: Wind tunnel experiments on the flow over rectangular cavities at subsonic and transonic speeds. Aeronaut. Res. Counc. Rep. Memoranda 3438 (1964)
Heller, H.H., Holmes, D.G., Covert, E.E.: Flow-induced pressure oscillations in shallow cavities. J. Sound Vib. 18(4), 545–553 (1971)
Heller, H.H., Bliss, D.B.: The physical mechanism of flow induced pressure fluctuations in cavities and concepts for their suppression. AIAA 75–491 (1975)
Lawson, S.J., Barakos, G.N.: Review of numerical simulations for high-speed, turbulent cavity flows. Prog. Aerosp. Sci. 47, 186–216 (2011)
Ben-Yakar, A., Hanson, R.K.: Cavity flameholders for ignition and flame stabilization in scramjets—review and experimental study. AIAA Pap. 98–3122 (1998)
Gruber, M.R., Baurle, R.A., Mathur, T., Hsu, K.Y.: Fundamental studies of cavity based flameholder concepts for supersonic combustors. J. Propul. Power 17(1), 146–153 (2001)
Vikramaditya, N.S., Kurian, J.: Pressure oscillations from cavities with ramp. AIAA J. 47(12), 2974–2984 (2009)
Murray, R.C., Elliot, G.S.: Characteristics of the compressible shear layer over a cavity. AIAA J. 39(5), 846–856 (2001)
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Maurya, P.K., Rajeev, C., Kumar, R.V., Aravind Vaidyanathan (2017). Effect of Aft Wall Offset on Supersonic Flow over Cavity. In: Saha, A., Das, D., Srivastava, R., Panigrahi, P., Muralidhar, K. (eds) Fluid Mechanics and Fluid Power – Contemporary Research. Lecture Notes in Mechanical Engineering. Springer, New Delhi. https://doi.org/10.1007/978-81-322-2743-4_5
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DOI: https://doi.org/10.1007/978-81-322-2743-4_5
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