Computational and experimental study of supersonic flow over axisymmetric cavities

Dissimile P.J.: Effect of planform aspect ratio on flow oscillations in rectangular cavities. J. Fluids Eng. 122, 32–38 (2000)

Stallings, R.L.: Experimental cavity pressure distribution at supersonic speeds. NASA technical paper 2683 (1987)

Rossiter, J.E.: Wind-tunnel experiments on flow over rectangular cavities at subsonic and transonic speeds. Aeronautical Research Council technical paper 3438 (1964)

Heller, H.H., Bliss, D.B.: The physical mechanism of flow-induced fluctuations in cavities and concepts for their suppression. AIAA-1975-491 2nd Aeroacoustics conference, Hampton, March (1975)

Tam C.-J., Orkwis P.D., Dissimile P.J.: On the tones and pressure oscillations induced by flow over rectangular cavities. J. Fluid Mech. 89, 373–399 (1978)

Unalmis O.H., Clemens N.T., Dolling D.S.: Cavity oscillation mechanisms in high-speed flows. AIAA J. 42, 2035–2041 (2004)

Mallinson S.G., Jackson A.P., Hillier R., Kirk D.C., Soltani S., Zanchetta M.: Gun tunnel flow calibration: defining input conditions for hypersonic flow computations. Shock Waves 10, 313–322 (2000)

Jackson A., Hillier R., Soltani S.: Experimental and computational study of laminar cavity flows at hypersonic speeds. J. Fluid Mech. 427, 329–358 (2001)

Hillier R. et al.: Development of some hypersonic benchmark flows using CFD and experiments. Shock Waves 13, 375–384 (2003)

Creighton, S.: Hypersonic flow over non-rectangular cavities. Thesis, Imperial College London, UK (2003)

Creighton S., Hillier R.: Experimental and computational study of unsteady hypersonic cavity flows. Aeronaut. J. 111, 673–688 (2007)

Murray, N., Hillier, R.: Axisymmetric separated shock-wave boundary-layer interaction. In: 26th International Symposium on Shock Waves, Goettingen (2007)

Menter, F.R.: Eddy viscosity transport equations and their relation to the k-epsilon model. NASA STI/Recon Technical Report no. 95 (1994)

Murray, N.: Three-dimensional turbulent shock-wave/boundary-layer interactions in hypersonic. Thesis, Imperial College London, UK (2006)

Denison M.R., Baum E.: Compressible free shear layer with finite initial thickness. AIAA J. 1, 342–349 (1963)

Kubota T., Dewey C.F.: Momentum integral methods for the laminar free shear layer. AIAA J. 2, 625–629 (1964)

Charwat, A., Der, J.: Studies on laminar and turbulent free shear layers with a finite initial boundary layer at separation. AGARD CP No. 4 (1966)

Bauer, R.C., Dix, R.E.: Engineering model of unsteady flow in a cavity. Arnold Engineering Development Center, AEDC-TR-17 (1975)

Cattafesta, L., Shukla, D., Garg, S., Ross, J.: Development of an adaptive weapons-bay suppression system. In: AIAA-1999-1901 5th Aeroacoustics Conference and Exhibit, Bellevue, May 1999

Kegerise M.A., Spina E.F., Garg S., Cattafesta L.N.: Mode-switching and nonlinear effects in compressible flow over a cavity. Am. Inst. Phys. 16, 678–687 (2004)

Ukeiley L., Ponton M., Seiner J., Jansen B.: Suppression of pressure loads in cavity flows. AIAA J. 42, 70–79 (2004)

Zhang X., Edwards J.A.: An investigation of supersonic oscillatory cavity flows driven by thick shear layers. Aeronaut. J. 94, 355–364 (1990)