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- [2] Flow visualization of supersonic transverse jet over Mach 2 freestream of a sharp cone Journal of Visualization, 2010, 13 : 79 - 80
- [4] Experimental investigation of a supersonic Mach 2.5 wall jet in a hypersonic Mach 6 crossflow: Sharp leading edge flat plate with laminar incoming boundary layer FOURTH INTERNATIONAL SYMPOSIUM ON EXPERIMENTAL AND COMPUTATIONAL AEROTHERMODYNAMICS OF INTERNAL FLOWS, VOL II, PROCEEDINGS, 1999, : 156 - 163
- [5] Computational study of the cavity flow over sharp nose cone in supersonic flow INTERNATIONAL JOURNAL OF MODERN PHYSICS C, 2020, 31 (06):