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Xin Zhang Zhang, X. & Edwards, J.A., "The effect of trailing edge geometry on cavity flow oscillation driven by a supersonic shear layer," The Aeronautical Journal, Vol. 102, No. 1013, March 1998, pp. 129-136. 1998
Xin Zhang Zhang, X., "Turbulence measurements of a longitudinal vortex generated by an inclined jet in a turbulent boundary layer," ASME Journal of Fluids Engineering, Vo. 120, December 1998, pp. 765-771. 1998
Xin Zhang Zhang, X. & Edwards, J.A., "Pressure over a two-cavity cascade at supersonic speeds oscillation driven by a supersonic shear layer," The Aeronautical Journal, Vol. 103, No. 1022, January 1999. pp. 45-54. 1998
Xin Zhang Zhang, H.L. & Zhang, X., Flow structure analysis around an oscillating circular cylinder at low KC number: a numerical study," Computers & Fluids, Vol. 26, No. 1, January 1997, pp. 83-106. 1997
Xin Zhang Lilley, G. M., Zhang, X. & Rona, A., "The progress in computational aeroacoustics in predicting the noise radiated from turbulent flow," International Journal of Acoustics and Vibration, Vol. 2, No. 1, March 1997. pp. 3-10. 1997
Xin Zhang Zhang, X. & Collins, M. W., "Measurements of a longitudinal vortex generated by a rectangular jet in a turbulent boundary layer" Physics of Fluids, 9(6), June 1997. pp. 1665-1673. 1997
Xin Zhang Zhang, X. & Collins, M. W., "Nearfield evolution of a longitudinal vortex generated by an inclined jet in a turbulent boundary layer," ASME Journal of Fluids Engineering, Vo. 119, December 1997, pp. 934-939. 1997
Xin Zhang Zhang, X. & Edwards, J.A., "Analysis of unsteady supersonic cavity flow employing an adaptive meshing refinement algorithm," Computers & Fluids, Vol. 25, No. 4, July 1996, pp. 373-393. 1996
Xin Zhang Zhang, X., Stasiek, J. & Collins, M. W., "Experimental and numerical analysis of convective heat transfer in turbulent channel flow with square and circular columns," Experimental Thermal and Fluid Science, Vol. 10, No. 2, January 1995, pp. 229-237. 1995
Xin Zhang Zhang, X., "Compressible flow oscillation due to shear layer instabilities and pressure feedback," AIAA Journal, Vol.33, No.8, August 1995, pp. 1404-1411. 1995