Journal Publications

  1. Im, H.-S. and Zha, G.-C., "Investigation of Flow Instability Mechanism Causing Compressor Rotor Blade Non-Synchronous Vibration", AIAA Journal, vol. 52, No. 9, pp. 2019-2031, 2014, DOI: http://arc.aiaa.org/doi/abs/10.2514/1.J052781
  2. Im, H.-S. and Zha, G.-C., "Delayed Detached Eddy Simulation of Airfoil Stall Flows Using High Order Schemes", ASME Journal of Fluids Engineering, 2014, DOI: 10.1115/1.4027813
  3. Wang, J., Bartow, W., Moreyra, A., Woyczynski, G. , G.-C. Zha, "Low Drag Automotive Mirrors Using Passive Jet Flow Control", SAE Int. J. Passeng. Cars - Mech. Syst. 7(2):2014, doi:10.4271/2014-01-0584
  4. Shen, Y.-Q., Zha, G.-C. , "Improvement of weighted essentially non-oscillatory schemes near discontinuities", Journal of Computer and Fluids, (2014), doi: http://dx.doi.org/10.1016/j.compfluid.2014.02.010
  5. Shen, Y.-Q., Zha, G.-C. , "Improvement of weighted essentially non-oscillatory schemes near discontinuities", Journal of Computer and Fluids, (2014), doi: http://dx.doi.org/10.1016/j.compfluid.2014.02.010
  6. Im, H.-S., Zha, G.-C. and Dano, B., "Large Eddy Simulation of Co-Flow Jet Airfoil at High Angle of Attack", Journal of Fluids Engineering, vol. 136(2), p. 021101, 2014
  7. Shen, Y.-Q., Zha, G.-C. and Huerta, M. A., "E-CUSP Scheme for the Equations of Ideal Magnetothydrodynamics with High Order WENO Scheme", Journal of Computational Physics, Vol. 231, No. 19, pp6233-6249, 2012
  8. Im, H.-S. and Zha, G.-C., " Detached Eddy Simulation of Rotating Stall Inception for a Full Annulus Transonic Rotor", AIAA Journal of Propulsion and Power, Vol. 28, No. 4, July/Aug 2012
  9. Shen, Y.-Q. and Zha, G.-C., “Low diffusion E-CUSP scheme with implicit high order WENO scheme for preconditioned Navier-Stokes equations", Journal of Computer & Fluids, Vol. 55, pp13-23, 2012
  10. Wang, B .-Y. and Zha, G.-C., "Detached-eddy simulation of transonic limit cycle oscillations using high order schemes", Journal of Computer and Fluids, Vol. 52, 58-68, 2011
  11. Wang, B.-Y and Zha, G.-C., "Detached-Eddy Simulation of a Co-Flow Jet Airfoil at High Angle of Attack", AIAA Journal of Aircraft, Vol. 48, No. 5, 2011
  12. Zha, G.-C., Shen, Y.-Q. and Wang, B.-Y., " An Improved Low Diffusion E-CUSP Upwind Scheme", Journal of Computer & Fluids,Vol. 48, pp 214–220, 2011
  13. Shen, Y.-Q. and Zha, G.-C., "Generalized finite compact difference scheme for shock/complex flowfield interaction", Journal of Computational Physics, 2011, 230, pp 4419–4436
  14. Shen, Y.-Q. and Zha, G.-C., "Large Eddy Simulation  Using a New Set of Sixth Order Schemes for Compressible Viscous Terms", Journal of Computational Physics, 2010, 229:8296-8312
  15. Wang, B.-Y. and Zha, G.-C., "Numerical simulation of transonic limit cycle oscillations using high-order low-diffusion schemes", Journal of Fluids and Structures, Vol, 26, pp 579–601, 2010
  16. Shen, Y.-Q., Zha, G.-C., "Improvement of the WENO Scheme Smoothness Estimator", International Journal for Numerical Methods in Fluids, 64:653–675, 2010
  17. Shen, Y.-Q., Zha, G.-C. and Xiangying Chen, "High Order Conservative Differencing for Viscous Terms and the Application to Vortex-Induced Vibration Flows", Journal of Computational Physics, 2009, 228(2):8283-8300
  18. Shen, Y.-Q. and Zha, G.-C. and Wang, B.-Y., "Improvement of Stability and Accuracy of Implicit WENO Scheme", AIAA Journal, Vol. 47, No. 2, 2009, pp331-344
  19. Wang, B.-Y., Hu, Z.-J. and Zha, G.-C., "A General Sub-Domain Boundary Mapping Procedure For Structured Grid CFD Parallel Computation", AIAA Journal of Aerospace Computing, Information, and Communication, Vol. 5, No. 11, Nov., pp425-447, 2008.
  20. Wang, B.-Y., Haddoukessouni, B., Levy, J. and Zha, G.-C., "Numerical Investigations of Injection Slot Size Effect on the Performance of Co-Flow Jet Airfoil", AIAA Journal of Aircraft, Vol. 45, No. 6, 2008, pp.2084-2091, PDF
  21. Zha, G.-C., Bruce F. Carroll, Paxton, C., Clark A. Conley and Adam Wells , "High Performance Airfoil Using Co-Flow Jet Flow Control ", AIAA Journal, Vol. 45, No. 8, pp.2087-2090, 2007, PDF
  22. Zha, G.-C., Gao, W. and Paxton, C. D. "Jet Effects on Co-Flow Jet Airfoil Performance ", AIAA Journal, Vol.45, No.6, 2007, pp1222-1231, PDF
  23. Chen, X.-Y. and Zha, G.-C. and Yang, M.-T. "Numerical Simulation of 3-D Wing Flutter with Fully Coupled Fluid-Structural Interaction ", Journal of Computers & Fluids, Vol. 36, No. 5, June 2007, pp856-867, PDF
  24. Zha, G.-C and Paxton, C. and Conley, A. and Wells, A. and Carroll, B. "Effect of Injection Slot Size on High Performance Co-Flow Jet Airfoil" AIAA Journal of Aircraft, Vol. 43, No. 4, pp987-995, 2006, PDF
  25. Zha, G.-C. and Paxton, C. "A Novel Flow Control Method for Airfoil Performance Enhancement Using Co-Flow Jet", Applications of Circulation Control Technologies, AIAA Book Series, Progress in Aeronautics and Astronautics, Vol. 214, 2006, Chapter 10, p. 293-314, Editors: R. D. Joslin and G. S. Jones
  26. Chen, X. and Zha, G.-C., "Implicit Application of Non-Reflective Boundary Conditions for Navier-Stokes Equations in Generalized Coordinates ", International Journal for Numerical Methods in Fluids, Vol. 50, No. 7, pp767-793, 2006
  27. Chen, X. and Zha, G.-C.,"Fully Coupled Fluid-Structural Interactions Using an Efficient High Solution Upwind Scheme", Journal of Fluid and Structure, Vol. 20, No. 8, Nov. 2005, pp1105-1125, PDF
  28. Zha, G.-C., "A Low Diffusion Efficient Upwind Scheme " , AIAA Journal, Vol.43, No.5, pp 1137-1140, 2005
  29. Hu, Z. and Zha, G.-C.,"Calculations of 3D Compressible Using an Efficient Low Diffusion Upwind Scheme",International Journal for Numerical Methods in Fluids, Vol. 47, pp253-269, Nov. 2005
  30. Zha, G.-C.,"Boundary Layer Loss Mechanism and Justification of Wall Functions for Turbulence Modeling" , AIAA Journal, Vol. 42, No. 11, Nov. 2004, p2387-2390
  31. Zha, G.-C. and Hu, Z.,"Calculation of Transonic Internal Flows Using an Efficient High Resolution Upwind Scheme" , AIAA Journal, Vol. 42, No. 2. 2004, pp205-214
  32. Zha, G.-C, "Numerical Tests of Upwind Scheme Performance for Entropy Condition", AIAA Journal, Vol. 37, No. 8, August 1999, p. 1005-1007
  33. Zha, G.-C., Knight, D. D., Smith, D., "Numerical Investigations of High Speed Civil Transport Inlet Unstart Transient at Angle of Attack", AIAA Journal of Aircraft, Vol. 35, No.6, Nov.-Dec., 1998, p. 851-856
  34. Zha, G.-C., Knight, D. D., Smith, D., and Haas, M., "Numerical Simulation of High Speed Civil Transport Inlet Operability with Angle of Attack", AIAA Journal, Vol. 36, No. 7, July, 1998, p. 1223-1229
  35. Zha, G.-C., Smith, D., Schwabacher, M., Rasheed, K., Gelsey, A., Knight, D. D. and Haas, M., "High Performance Supersonic Missile Inlet Design Using Automated Optimization", AIAA Journal of Aircraft, Vol.34, No. 6, Nov.-Dec. 1997, p. 697-705
  36. Zha, G.-C., and Knight, D. D., " Computation of 3D Shock/Turbulent Boundary Layer Interaction Using a Reynolds Stress Equation Turbulence Model", AIAA Journal, Vol. 34, No.7, July 1996, p. 1313-1320
  37. Zha, G.-C. and Bilgen, E., " Numerical Study of Three-Dimensional Transonic Flows Using Unfactored Upwind- Relaxation Sweeping Algorithm", Journal of Computational Physics, Vol. 125, No. 2, May 1996, p. 425-433
  38. Zha, G.-C. and Bilgen, E., " Numerical Solutions of Euler Equations by Using a New Flux Vector Splitting Scheme", International Journal for Numerical Methods in Fluids, Vol. 17, 1993, p. 115-144
  39. Liu, D.-Z. and Zha, G.-C., "Transonic Flow Calculation of Euler Equations by Implicit Iterating Scheme with Flux Splitting", Acta Aeronautica et Astronautics Sinica, Vol. 11, No.9, 1990, p. A449-455
  40. Zha, G.-C., Liu, D.-Z. and Ma, T.-U., " An Efficient Upwind-Relaxation Algorithm for Euler and Navier-Stokes Equations", International Journal for Numerical Methods in Fluids, Vol. 9, No. 5, 1989, p. 517-529
  41. Zha, G.-C. and Yan, R.-Q., "Investigations of the Performance of the Supersonic Multiple Circular Arc (MCA) Airfoil Cascades of Axial-Flow Compressors", Journal of Aerospace Power, Vol. 2, No. 2, April 1987, p. 113-118