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## Complete list of publications | ||

1988-2000 | 2000-2005 | 2005-2010 | 2010-2012 | 2012-2013 |

1988 | ||

1) | Zhang, X. & Edwards, J. A., "Computational analysis of unsteady cavity flows driven by thick shear layers," The Aeronautical Journal, Vol. 92, No. 919, November 1988, pp. 350-373. | |

2) | Zhang, X. & Edwards, J. A., "An investigation of supersonic oscillatory cavity flows driven by a thick shear layer," The Aeronautical Journal, Vol. 94, No. 940, December 1990, pp. 353-364. | |

3) | Zhang X. & Edwards, J. A., "An experimental investigation of supersonic flow over two cavities in tandem," AIAA Journal, Vol. 30, No. 5, May 1992, pp. 1182-1190. | |

4) | Zhang, X. & Collins, M. W., "Flows and heat transfer in a turbulent boundary layer through skewed and pitched jets," AIAA Journal, Vol. 31, No. 9, September 1993. pp. 1590-1599. | |

5) | Zhang, X. & Ing, D., "Computational analysis of a single jet impingement ground effect lift loss," Journal of Aircraft, Vol. 31, No. 2, February 1994, pp. 256-262. | |

6) | Ing, D. & Zhang, X., "An experiment and computational investigation of ground effect lift loss for single jet impingement," The Aeronautical Journal, Vol. 98, No. 974, April 1994, pp. 127-136. | |

7) | 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. | |

8) | Zhang, X., "Compressible flow oscillation due to shear layer instabilities and pressure feedback," AIAA Journal, Vol.33, No.8, August 1995, pp. 1404-1411. | |

9) | Zhang, X, "Co- and Contra-rotating streamwise vortices in a turbulent boundary layer", Journal of Aircraft, Vol. 32, No. 5, September-October 1995, pp. 1095-1101. | |

10) | 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. | |

11) | 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. | |

12) | 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. | |

13) | 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. | |

14) | 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. | |

15) | Zhang, X., Rona, A., & Edwards, J.A., "An observation of pressure waves around a shallow cavity," Journal of Sound and Vibration, 214(4), 1998, pp. 771-778. | |

16) | 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. | |

17) | 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. | |

18) | 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. | |

19) | Zhang, X., Chen, X., Rona, A., & Edwards, J.A., "Attenuation of cavity flow oscillation through leading edge flow control," Journal of Sound and Vibration, 221(1), March 1999, pp. 21-47. | |

20) | Zhang, X., "Contra-rotating vortices embedded in a turbulent boundary layer with inclined jets," AIAA Journal. Vol. 37, No.10, October 1999. pp. 1277-1284. | |

21) | Jeffrey, D.R., Zhang, X. & Hurst, D.W., "Aerodynamics of Gurney flaps on a single-element high-lift wing," Journal of Aircraft. Vol. 37, No. 2, March-April 2000. pp. 295-302. | |

2000 | ||

22) | Zhang, X., "An inclined rectangular jet in a turbulent boundary layer," Experiments in Fluids. 28(4), April 2000, pp. 344-354. | |

23) | Zhang, X., "Turbulence measurements of an inclined rectangular jet in a boundary layer," International Journal of Heat and Fluid Flow. 21(3), May 2000, pp. 291-296. | |

24) | Zerihan, J. & Zhang, X., "Aerodynamics of a single-element wing-in-ground effect," Journal of Aircraft, Vol. 37, No. 6, November-December 2000, pp. 1058-1064 | |

25) | Jeffrey, D.R., Zhang, X. & Hurst, D.W., "Some aspects of aerodynamics of Gurney flaps on a double-element wing," ASME Journal of Fluids Engineering, Vol. 123, No.1, March, 2001, pp. 99-104. | |

26) | Zhang, X. & Senior, A., "Force and pressure of a diffuser equipped bluff body in ground effect," ASME Journal of Fluids Engineering. Vol. 123, No. 1, March 2001, 105-111. ( doi: 10.1115/1.1340637) | |

27) | Zhang, X. & Zerihan, J., "Aerodynamics of Gurney flaps on a wing in ground effect," AIAA Journal, Vol. 39, No. 5, May 2001, pp. 772-780. | |

28) | Ashcroft, G. & Zhang, X., "Optimized prefactored compact schemes," Journal of Computational Physics, Vol. 190, 2003, pp. 459-477. | |

29) | Zhang, X. & Zerihan, J., "Aerodynamics of a double element wing in ground effect," AIAA Journal, Vo. 45, No. 6, June 2003, pp. 1007-1016. | |

30) | Ashcroft, G., Takeda, K, & Zhang, X., "A numerical investigation of noise radiated by a turbulent flow over a cavity", Journal of Sound and Vibration, 265(1), 31 July 2003, pp. 43-60. | |

31) | Ruhrmann A., & Zhang, X., "Influence of diffuser angle on a bluff body in ground effect," ASME Journal of Fluids Engineering. Vol. 125, No. 2, March 2003, pp. 332-338. | |

32) | Zhang, X. & Zerihan, J., "Off-surface aerodynamic measurements of a wing in ground effect," Journal of Aircraft, Vol. 40, No. 4, July-August 2003, pp. 716-725. | |

33) | Zhang, X., "Evolution of co-rotating vortices in a canonical boundary layer with inclined jets," Physics of fluids, 15(12), 2003, pp. 3693-3702. | |

34) | Chen, X.X., Zhang, X., Morfey, C.L. & Nelson, P.A., "A numerical method for noise radiation from an unflanged duct", Journal of Sound and Vibration, 270, 2004, pp. 573-586. | |

35) | Richards, S, Zhang, X. & Nelson, P.A., "The evaluation of a buffer zone as an inflow/outflow boundary condition for computational aeroacoustic applications," Journal of Sound and Vibration, 270, 2004, pp. 539-557. | |

36) | Takeda, K., Zhang, X., Morfey, C.L. & Nelson, P.A., "Computational aeroacoustic simulation of leading edge slat flow," Journal of Sound and Vibration, Vol. 270, 2004, pp. 559-572. | |

37) | Rona, A. & Zhang, X., "Time accurate numerical study of turbulent supersonic jets", Journal of Sound and Vibration, 270(1-2), 6 February 2004, Pages 297-321 | |

38) | Zhang, X., Senior, A., & Ruhrmann, "Vortices behind a bluff body with an upswept aft section in ground effect," International Journal of Heat and Fluid Flow, 25(1), 2004, pp. 1-9. | |

39) | Zhang, X. & Zerihan, J., "Edge vortices of a double element wing in ground effect," Journal of Aircraft, Vol. 41, No. 5, pp. 1127-1137, 2004. | |

40) | Zhang, X., Chen, X.X., Morfey, C.L. and Nelson, P.A., "Computation of spinning modal of radiation from an unflanged duct," AIAA Journal, Vol. 42, No. 9, September 2004, pp. 1795-1801. | |

2005 | ||

41) | Ashcroft, G. and Zhang, X., "Vortical structures over rectangular cavities at low speed", Physics of fluids, Vol 17, January 2005, pp. 015104-1:8. | |

42) | Mahon, S. & Zhang, X., "Computational analysis of pressure and wake characteristics of an airfoil in ground effect," ASME Journal of Fluids Engineering, 127(2), March 2005, pp. 290-298. | |

43) | Zhang, X., Chen, X.X., Morfey, C.L., "Acoustic radiation from a semi-infinite duct with a Subsonic Jet," International Journal of Aeroacoustics, 4(1), January 2005, pp. 169-184. | |

44) | Pattenden, R., Turnock, S. & Zhang, X., "Measurements of the flow over a low aspect-ratio cylinder mounted on a ground plane," Experiments in Fluids, 39(1), July 2005, pp. 10-21. | |

45) | Zhang, X., Toet, W. and Zerihan, J., "Ground effect aerodynamics of racing cars", Applied Mechanics Review, 59(1), January 2006, pp. 33-49. (doi:10.1115/1.2110263) | |

46) | McManus, J. & Zhang, X., "A computational study of the flow around an isolated wheel in contact with ground," ASME Journal of Fluids Engineering, 128(3), May 2006, pp. 520-530. | |

47) | Huang, X. and Zhang, X., "A Fourier pseudospectral method for some computational aeroacoustics Problems," International Journal of Aeroacoustics, 5(3), September 2006, pp. 279-294. | |

48) | Mahon, S. & Zhang, X., "Computational analysis of a double element airfoil in ground effect,"ASME Journal of Fluids Engineering, 128(6), November 2006, pp. 1172-1180. | |

49) | Ma, Z.K., Smith, M.G., Richards, S.K., and Zhang, X., "Attenuation of slat trailing edge noise using acoustic liners," International Journal of Aeroacoustics, 5(4), 2006, pp. 311-333. | |

50) | Zhang, X. and Toet, W., "Ground effect aerodynamics research of racing cars", AutoTechnology, 6, December 2006, pp. 40-43. | |

51) | Nishino, T., Roberts, G. and Zhang, X., "Vortex shedding from a circular cylinder near a moving ground," Physics of Fluids, Vol. 19, February 2007, 025103, 12pp. (doi:10.1063/1.2710273) | |

52) | Chan, S., Zhang, X. and Gabriel, S., "Attenuation of low-speed flow-induced cavity tones using plasma actuators," AIAA Journal, 45(7), July 2007, pp. 1525-1538. | |

53) | Richards, S, Chan, X., Huang, X and Zhang, X., "Computation of fan noise radiation through an engine exhaust geometry with flow," International Journal of Aeroacoustics, 6(3), 2007, pp. 223-241. | |

54) | Huang, X., Chan, X., and Zhang, X., "Atmospheric plasma actuators for aeroacoustic applications," IEEE Transaction on Plasma Sciences, 35(3), June 2007, pp.693-695. | |

55) | Zhang, X., P. Blyth, P. Dunning, M. Gardner, C. Wood, "Aerodynamic model of a hill climb racing car," Bernoulli Aerodynamics International, 2(5), August 2007, pp.52-61. | |

56) | Nishino, T., Roberts, G. and Zhang, X., "Unsteady RANS and detached-eddy simulations of flow around a circular cylinder subject to ground effect," Journal of Fluids and Structures, 24(1), January, 2008, pp. 18-33. (doi:10.1016/j.jfluidstructs.2007.06.002) | |

57) | Huang, X., Chan, S., Zhang, X. and, S. Gabriel, "Variable structure model for flow-induced tonal noise control with plasma actuators", AIAA Journal, 46(1), January 2008, pp. 241-250. | |

58) | Huang, Xun, Chen, Xiaoxian, Ma, Zhaokai and Zhang, Xin, "Efficient computation of spinning modal radiation through an engine bypass duct", AIAA Journal, 46(6), June 2008, pp. 1413-1423. | |

59) | Huang, Xun and Zhang, Xin, "Streamwise and spanwise plasma actuators for flow-induced cavity noise control. Physics of Fluids," 20 (3), 2008, 037101-[10pp]. (doi:10.1063/1.2890448). | |

60) | Huang, X., Zhang, X., Richards, S.K, "Adaptive mesh refinement computation of acoustic radiation from an engine Intake," Aerospace Sciences and Technology, 12(5), July 2008, pp. 418-426.( doi:10.1016/j.ast.2007.09.004) | |

61) | Chen, X., Huang, X. and Zhang, X. "Sound radiation from a bypass duct with bifurcations," AIAA Journal, 47(2), February 2009, pp. 429-436. | |

62) | Boorsma, K., Zhang, X. and Molin, N., "Bluff body noise control using perforated fairings," AIAA Journal, 47(1), January 2009, pp. 33-43. | |

63) | Angland, D., Zhang, X. and Molin, N., "Measurements of flow around a flap side edge with porous edge treatment," AIAA Journal, 47(7), July 2009, pp. 1660-1671, (doi: 10.2514/1.39311). | |

64) | Van Den Berg, M. and Zhang, X., "The aerodynamic interaction between an inverted wing and a rotating wheel," ASME Journal of Fluids Engineering, 131(10), October 2009, 101104, (doi:10.1115/1.3215942) (13 pages). | |

65) | Kuya, Y , Takeda, K., Zhang, X., "Flow physics of a race car wing with vortex generators in ground effect," ASME Journal of Fluids Engineering, 131(12), December 2009, 121103, (doi:10.1115/1.4000423) (9 pages) | |

66) | Kuya, Y , Takeda, K., Zhang, X., "Flow separation control on a race car wing with vortex generators in ground effect ," ASME Journal of Fluids Engineering, 131(12), December 2009, 121102, (doi:10.1115/1.4000420) (8 pages) | |

67) | Ma, Z.K. and Zhang, X., "Numerical investigation of broadband slat noise attenuation with acoustic liner treatment," AIAA Journal, 47(12), December 2009, pp. 2812-2820. | |

2010 | ||

68) | Li, Y., Zhang, X. and Huang X., "The use of plasma actuators for bluff body broadband noise control," Experiments in Fluids, January 2010, (doi: 10.1007/s00348-009-0806-3). | |

69) | Kuya, Y , Takeda, K., Zhang, X., "Computational investigation of a race car wing with vortex generators in ground effect ," ASME Journal of Fluids Engineering, 132(2), February 2010, 021102, (doi: 10.1115/1.4000741) (8 pages). | |

70) | Huang, X. and Zhang, X., "Plasma actuators for noise control," International Journal of Aeroacoustics, 2010, 9(4-5), pp. 679-704. | |

71) | Li, Y., Zhang, X. and Smith, M. G., "Identification and attenuation of a tonal-noise source on an aircraft landing gear," Journal of Aircraft, 47(3), May-June 2010. pp. 796-805. (doi: 10.2514/1.43183). (10 pages). | |

72) | Boorsma, K., Zhang, X. and Molin, N., "Landing gear noise control using perforated fairings," Acta Mech Sin, 26(2), 2010, pp 159-174. (doi: 10.1007/s10409-009-0304-0). | |

73) | Li, Y., Zhang, X. and Smith, M. G., "Measurements and control of aircraft"s main landing gear broadband noise," Aerospace Sciences and Technology, July 2011, (doi:10.1016/j.ast.2011.07.009) | |

74) | Huang, X. and Zhang, X., "Broadband flow-induced sound control using plasma actuators," Journal of Sound and Vibration, 329(13), 21 June 2010, Pages 2477-2489. (doi: 10.1016/j.jsv.2010.01.018) | |

75) | Peers, E.; Zhang, X. and Kim, J. W., " Patched characteristic interface condition for high-order multiblock aeroacoustic computation," AIAA Journal, 48(11), November 2010, pp. 2512-2522, (doi: 10.2514/1.J050130). | |

76) | Kuya, Y , Takeda, K., Zhang, X., Forrester, A. "Multifidelity surrogate modeling of experimental and computational aerodynamic data sets" AIAA Journal, 49(2), February 2011, pp. 289-298. (doi: 10.2514/1.J050384) | |

77) | Zhang, X., "Airframe noise: high lift device noise," in Encyclopedia of Aerospace Engineering, Edited by Blockley, R. and Shyy, W., ISBN 978-0-470-75440-5, Willy, 6, pp.3541-3551 | |

78) | Cui, E. J. and Zhang, X., "Ground effect aerodynamics," in Encyclopedia of Aerospace Engineering, Edited by Blockley, R. and Shyy, W., ISBN 978-0-470-75440-5, Willy, 1, pp.246-256 | |

79) | Molina, J. and Zhang, X., "Aerodynamic motion and stability of a heaving airfoil in ground effect," ACTA Mechanica Sinica, 27(2), 2011 | |

80) | Molina, J. and Zhang, X., "Aerodynamics of a heaving airfoil in ground effect," AIAA Journal, 49, 2011, (doi: 10.2514/1.J050369) | |

81) | Zhang, X., "Aircraft noise and its nearfield propagation computations," Acta Mechanica Sinica, 2012, (4): 960-977. (doi: 10.1007/s10409-012-0136-1 | |

82) | Angland, D., Zhang, X. and Goodyer, M., "The use of blowing flow control to reduce bluff body interaction noise," AIAA Journal, 2012, 50, (8), 1670-1684. (doi:10.2514/1.J051074). | |

2013 | ||

83) | Chen, X. X. and Zhang, X., "High-Order Interface for Aeroacoustic Computation Using Overset Grid," AIAA Journal, 51(2), February, 2013, pp. 519-523. (doi: 10.2514/1.J051810) | |

84) | Zhou, Jie, Bhaskar, A., Zhang, X., "Sound transmission through a double-panel construction lined with poroelastic material in the presence of mean flow," Journal of Sound and Vibration, (2013), (doi: 10.1016/j.jsv.2013.02.020) | |

85) | Liu, W., Kim, J. W., Zhang, X., Angland, D., Caruelle, B., "Landing-gear noise prediction using high-order finite difference schemes," Journal of Sound and Vibration, Volume 332, Issue 14, 8 July 2013, Pages 3517-3534, (doi: 10.1016/j.jsv.2013.01.035. ) | |

86) | Chen, P., Zhang, X., Chappell, S., Cai, Z., and Angland, D., "Attenuation of noise from an airfoil equipped with a high-lift device using plasma actuators," ERCOFTAC Bulletin, Vol. 94, 2013, pp. 65-69. | |

87) | Zhou, Jie, Bhaskar, A., Zhang, X., "Optimization of sound transmission through a double-wall panel," 74 Applied Acoustics, 74 (2013), pp. 1422-1428. (doi: 2013.06.002) | |

88) | Wang, Cindy, Hu, Zhiwei and Zhang, X., "Aeroacoustic effects of high-lift wing slat track and cut-out system," International Journal of Aeroacoustics, 12(3) 2013, pp. 283-308. | |

89) | Gill, James, Zhang, Xin, and Joseph, Phil, "Symmetrci airfoil geometry effects on airfoil leading edge noise," Journal of the Acoustical Society of America, accepted. | |

90) | Zhang, Xin and Chen, Xiaoxian, "Broadband Wave Propagation from an Aero-engine Duct," AIAA Journal, accepted. | |

91) | Cai, Z., Chen, P., Angland, D. and Zhang, Xin, Active flow separation control by positional based iterative learning control," International Journal of Control, accepted. |