Anderson, G., Kumar, A. & Erdos, J.
1990
Progress in hypersonic combustion technology with computation and experiment.
AIAA Paper 90-5254.
Anyiwo, J. C. & Bushnell, D. M.
1982
Turbulence amplification in shock-wave boundary layer interaction.
AIAA J.
20,
893–899.
Buttsworth, D. R.
1994
Shock induced mixing and combustion in scramjets. PhD thesis,
Department of Mechanical Engineering, The University of Queensland.
Drummond, J. P.
1991
Mixing enhancement of reacting parallel fuel jets in a supersonic combustor.
AIAA Paper 91-1914.
Drummond, J. P., Carpenter, M. H. & Riggins, D. W.
1991
Mixing and mixing enhancement in supersonic reacting flowfields. In
High-Speed Flight Propulsion Systems (ed.S. N. B. Murthy & E. T. Curran).
Progress in Astronautics and Aeronautics, vol. 137, pp.
383–455.
AIAA.
Fernando, E. M. & Menon, S.
1993
Mixing enhancement in compressible mixing layers: an experimental study.
AIAA J.
31,
278–285.
Gilreath, H. E. & Sullins, G. A.
1989 Investigation of the mixing of parallel supersonic streams. ISABE Paper 89-7060.
Guirguis, R. H.
1988
Mixing enhancement in supersonic shear layers: III. Effect of convective Mach number.
AIAA Paper 88-0701.
Hall, J. L., Dimotakis, P. E. & Roseman, H.
1993
Experiments in nonreacting compressible shear layers.
AIAA J.
31,
2247–2254.
Hayes, W. D.
1957
The vorticity jump across a gasdynamic discontinuity.
J. Fluid Mech.
2,
595–600.
Hayes, W. D. & Probstien, R. F.
1959 Hypersonic Flow Theory, 1st edn.
Academic press.
Henderson, L. F.
1967
The reflexion of a shock wave at a rigid wall in the presence of a boundary layer.
J. Fluid Mech.
30,
699–722.
Hyde, C. R., Smith, B. R., Schetz, J. A. & Walker, D. A.
1990
Turbulence measurements for heated gas slot injection in supersonic flow.
AIAA J.
28,
1605–1614.
Kumar, A., Bushnell, D. M. & Hussaini, M. Y.
1989
Mixing augmentation technique for hypervelocity scramjets.
J. Propulsion Power
5,
514–522.
Li, C., Kailasanath, K. & Book, D. L.
1991
Mixing enhancement by expansion waves in supersonic flows of different densities.
Phys. Fluids A
3,
1369–1373.
Liepmann, H. W. & Roshko, A.
1957
Elements of Gasdynamics.
Wiley.
Lighthill, M. J.
1957
Dynamics of a dissociating gas. Part 1. Equilibrium flow.
J. Fluid Mech.
2,
1–32.
Marble, F. E., Hendricks, G. J. & Zukoski, E. E.
1987
Progress toward shock enhancement of supersonic combustion processes.
AIAA Paper 87-1880.
Marble, F. E., Zukoski, E. E., Jacobs, J. W. & Hendricks, G. J.
1990
Shock enhancement of and control of hypersonic mixing and combustion.
AIAA Paper 90-1981.
Menon, S.
1989
Shock-wave-induced mixing enhancement in scramjet combustors.
AIAA Paper 89-0104.
McKenzie, J. F. & Westphal, K. O.
1968
Interaction of linear waves with oblique shocks.
Phys. Fluids
11,
2350–2362.
Morkovin, M. V.
1960
Note on the assessment of flow disturbances at a blunt body travelling at supersonic speeds owing to flow disturbances in free stream.
Trans ASME E: J. Appl. Mech.
27,
223–229.
Northam, G. B. & Anderson, G. Y.
1986
Supersonic combustion ramjet research at Langley.
AIAA Paper 86-0159.
Northam, G. B., Capriotti, D. P., Byington, C. S. & Greenberg, I.
1991 Supersonic mixing and combustion in scramjets. ISABE Paper 91-7095.
Randolph, H., Chew, L. & Johari, H.
1994
Pulsed jets in supersonic crossflow.
J. Propulsion Power
10,
746–748.
Ribner, H. S.
1987
Spectra of noise and amplified turbulence emanating from shock-turbulence interaction.
AIAA J.
25,
436–442.
Riley, N.
1959
Interaction of a shock wave with a mixing region.
J. Fluid Mech.
7,
321–339.
Roshko, A. & Thomke, G. J.
1970
Supersonic, turbulent boundary-layer interaction with a compression corner at very high Reynolds number. In
Viscous Interaction Phenomena in Supersonic and Hypersonic Flow, pp.
109–138. University of Dayton Press, Ohio.
Roy, G. D.
1991 Subsonic and supersonic mixing and combustion enhancement. ISABE Paper 91-7093.
Schadow, K. C., Gutmark, E. & Wilson, K. J.
1990
Compressible spreading rates of supersonic coaxial jets.
Exps. Fluids
10,
161–167.
Shau, Y. R. & Dolling, D. S.
1992
Exploratory study of turbulent structure of a compressible shear layer using fluctuating Pitot pressure measurements.
Exps. Fluids
12,
293–306.
Shau, Y. R., Dolling, D. S. & Choi, K. Y.
1993
Organized structure in a compressible turbulent shear layer.
AIAA J.
31,
1398–1405.
Sullins, G. A., Gilreath, H. E., Mattes, L. A., King, P. S. & Schetz, J. A.
1991 Instabilities in confined supersonic mixing layers. ISABE Paper 91-7096.
Tillman, T. G., Patrick, W. P. & Paterson, R. V.
1991
Enhanced mixing of supersonic jets.
J. Propulsion Power
7,
1006–1014.
Truesdell, C.
1952
On curved shocks in steady plane flow of an ideal fluid.
J. Aero. Sci.
19,
826–828.
Vasilev, V. I., Zakotenko, S. N., Kraskeninnikov, S. Ju & Stepanov, V. A.
1994
Numerical investigation of mixing augmentation behind oblique shock waves.
AIAA J.
32,
311–316.
Waitz, I. A., Marble, F. E. & Zukoski, E. E.
1993
Investigation of a contoured wall injector for hypervelocity mixing augmentation.
AIAA J.
31,
1014–1021.
Yang, J., Kubota, T. & Zukoski, E. E.
1993
Applications of shock-induced mixing to supersonic combustion.
AIAA J.
31,
854–862.
