GeCheng Zha

Professor

  • 1947 Citations
1989 …2020

Research output per year

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Research Output

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Article
2020

Large eddy simulation of base drag reduction using jet boat tail passive flow control

Yang, Y., Bartow, W. B., Zha, G., Xu, H. & Wang, J., Feb 15 2020, In : Computers and Fluids. 198, 104398.

Research output: Contribution to journalArticle

2018

Full-Annulus simulation of nonsynchronous blade vibration excitation of an axial compressor

Espinal, D., Im, H. S. & Zha, G., Mar 1 2018, In : Journal of Turbomachinery. 140, 3, 031008.

Research output: Contribution to journalArticle

3 Scopus citations

Near-field sonic-boom prediction and analysis with hybrid grid Navier-Stokes solver

Ma, B., Wang, G., Ren, J., Ye, Z., Lei, Z. & Zha, G., Jan 1 2018, In : Journal of Aircraft. 55, 5, p. 1890-1904 15 p.

Research output: Contribution to journalArticle

3 Scopus citations
2017

Delayed detached Eddy simulation of wing flutter boundary using high order schemes

Gan, J. Y., Im, H. S., Chen, X. Y., Zha, G. C. & Pasiliao, C. L., May 1 2017, In : Journal of Fluids and Structures. 71, p. 199-216 18 p.

Research output: Contribution to journalArticle

4 Scopus citations

Truck Rear View Mirror Drag Reduction Using Passive Jet Boat Tail Flow Control

Gan, J., Li, L., Zha, G. & Czlapinski, C., Mar 28 2017, In : SAE Technical Papers. 2017-March, March

Research output: Contribution to journalArticle

2016

Performance and energy expenditure of coflow jet airfoil with variation of Mach number

Lefebvre, A., Dano, B., Bartow, W. B., Fronzo, M. D. & Zha, G. C., Jan 1 2016, In : Journal of Aircraft. 53, 6, p. 1757-1767 11 p.

Research output: Contribution to journalArticle

20 Scopus citations
2015

Bluff Body Drag Reduction Using Passive Flow Control of Jet Boat Tail

Hirst, T., Li, C., Yang, Y., Brands, E. & Zha, G., Sep 27 2015, In : SAE International Journal of Commercial Vehicles. 8, 2, p. 713-721 9 p.

Research output: Contribution to journalArticle

5 Scopus citations

Large Eddy Simulation of Base Drag Reduction with Jet Boat-Tail Passive Flow Control

Yang, Y., Xu, H., Wang, J. & Zha, G., 2015, In : Unknown Journal. 126, p. 150-157 8 p.

Research output: Contribution to journalArticle

1 Scopus citations
2014

Delayed Detached Eddy Simulation of Airfoil Stall Flows Using High-Order Schemes

Im, H. S. & Zha, G., Nov 1 2014, In : Journal of Fluids Engineering, Transactions of the ASME. 136, 11, 111104.

Research output: Contribution to journalArticle

14 Scopus citations

Improvement of weighted essentially non-oscillatory schemes near discontinuities

Shen, Y. & Zha, G., Jun 13 2014, In : Computers and Fluids. 96, p. 1-9 9 p.

Research output: Contribution to journalArticle

22 Scopus citations

Investigation of flow instability mechanism causing compressor rotor-blade nonsynchronous vibration

Im, H. & Zha, G., Sep 2014, In : AIAA journal. 52, 9, p. 2019-2031 13 p.

Research output: Contribution to journalArticle

5 Scopus citations

Large eddy simulation of coflow jet airfoil at high angle of attack

Im, H. S., Zha, G. C. & Dano, B. P. E., Jan 1 2014, In : Journal of Fluids Engineering, Transactions of the ASME. 136, 2, 4025649.

Research output: Contribution to journalArticle

21 Scopus citations

Low Drag Automotive Mirrors Using Passive Jet Flow Control

Wang, J., Bartow, W., Moreyra, A., Woyczynski, G., Lefebvre, A., Carrington, E. & Zha, G., Aug 2014, In : SAE International Journal of Passenger Cars - Mechanical Systems. 7, 2, p. 538-549 12 p.

Research output: Contribution to journalArticle

6 Scopus citations
2012

Detached-eddy simulation of rotating stall inception for a full-annulus transonic rotor

Im, H., Chen, X. Y. & Zha, G., Jul 1 2012, In : Journal of Propulsion and Power. 28, 4, p. 782-798 17 p.

Research output: Contribution to journalArticle

33 Scopus citations

E-CUSP scheme for the equations of ideal magnetohydrodynamics with high order WENO Scheme

Shen, Y., Zha, G. & Huerta, M. A., Aug 1 2012, In : Journal of Computational Physics. 231, 19, p. 6233-6247 15 p.

Research output: Contribution to journalArticle

20 Scopus citations

Low diffusion E-CUSP scheme with implicit high order WENO scheme for preconditioned Navier-Stokes equations

Shen, Y. & Zha, G., Feb 15 2012, In : Computers and Fluids. 55, p. 13-23 11 p.

Research output: Contribution to journalArticle

10 Scopus citations
2011

An improved low diffusion E-CUSP upwind scheme

Zha, G. C., Shen, Y. & Wang, B., Sep 1 2011, In : Computers and Fluids. 48, 1, p. 214-220 7 p.

Research output: Contribution to journalArticle

88 Scopus citations

Detached-eddy simulation of a coflow jet airfoil at high angle of attack

Wang, B. & Zha, G. C., 2011, In : Journal of Aircraft. 48, 5, p. 1495-1502 8 p.

Research output: Contribution to journalArticle

21 Scopus citations

Detached-eddy simulation of transonic limit cycle oscillations using high order schemes

Wang, B. & Zha, G. C., Dec 30 2011, In : Computers and Fluids. 52, 1, p. 58-68 11 p.

Research output: Contribution to journalArticle

18 Scopus citations

Generalized finite compact difference scheme for shock/complex flowfield interaction

Shen, Y. & Zha, G., Jun 1 2011, In : Journal of Computational Physics. 230, 12, p. 4419-4436 18 p.

Research output: Contribution to journalArticle

47 Scopus citations
2010

Improvement of the WENO scheme smoothness estimator

Shen, Y. & Zha, G., Oct 30 2010, In : International Journal for Numerical Methods in Fluids. 64, 6, p. 653-675 23 p.

Research output: Contribution to journalArticle

50 Scopus citations

Large eddy simulation using a new set of sixth order schemes for compressible viscous terms

Shen, Y. & Zha, G., Nov 2010, In : Journal of Computational Physics. 229, 22, p. 8296-8312 17 p.

Research output: Contribution to journalArticle

44 Scopus citations

Numerical simulation of transonic limit cycle oscillations using high-order low-diffusion schemes

Wang, B. & Zha, G. C., May 1 2010, In : Journal of Fluids and Structures. 26, 4, p. 579-601 23 p.

Research output: Contribution to journalArticle

23 Scopus citations
2009

Flow control of an airfoil via injection and suction

Chng, T. L., Rachman, A., Tsai, H. M. & Zha, G. C., Jan 1 2009, In : Journal of Aircraft. 46, 1, p. 291-300 10 p.

Research output: Contribution to journalArticle

29 Scopus citations

High order conservative differencing for viscous terms and the application to vortex-induced vibration flows

Shen, Y., Zha, G. & Chen, X., Dec 1 2009, In : Journal of Computational Physics. 228, 22, p. 8283-8300 18 p.

Research output: Contribution to journalArticle

77 Scopus citations

Improvement of stability and accuracy for weighted essentially nonoscillatory scheme

Shen, Y., Zha, G. & Wang, B., Feb 1 2009, In : AIAA journal. 47, 2, p. 331-344 14 p.

Research output: Contribution to journalArticle

104 Scopus citations
2008

General ndary mapping procedure for structured licit CFD parallel computation

Wang, B., Hu, Z. & Zha, G. C., Nov 1 2008, In : Journal of Aerospace Computing, Information and Communication. 5, 11, p. 425-447 23 p.

Research output: Contribution to journalArticle

55 Scopus citations

Numerical investigations of injection-slot-size effect on the performance of coflow jet airfoils

Wang, B., Haddoukessouni, B., Levy, J. & Zha, G. C., 2008, In : Journal of Aircraft. 45, 6, p. 2084-2091 8 p.

Research output: Contribution to journalArticle

40 Scopus citations
2007

High-performance airfoil using coflow jet flow control

Zha, G. C., Carroll, B. F., Paxton, C. D., Conley, C. A. & Wells, A., Aug 1 2007, In : AIAA journal. 45, 8, p. 2087-2090 4 p.

Research output: Contribution to journalArticle

59 Scopus citations

Jet effects on coflow jet airfoil performance

Zha, G. C., Gao, W. & Paxton, C. D., Jun 2007, In : AIAA journal. 45, 6, p. 1222-1231 10 p.

Research output: Contribution to journalArticle

59 Scopus citations

Numerical simulation of 3-D wing flutter with fully coupled fluid-structural interaction

Chen, X., Zha, G. C. & Yang, M. T., Jun 1 2007, In : Computers and Fluids. 36, 5, p. 856-867 12 p.

Research output: Contribution to journalArticle

68 Scopus citations
2006

Effect of injection slot size on the performance of coflow jet airfoil

Zha, G. C., Paxton, C. D., Conley, C. A., Wells, A. & Carroll, B. F., 2006, In : Journal of Aircraft. 43, 4, p. 987-995 9 p.

Research output: Contribution to journalArticle

51 Scopus citations
12 Scopus citations
2005

Calculations of 3D compressible flows using an efficient low diffusion upwind scheme

Hu, Z. & Zha, G., Jan 30 2005, In : International Journal for Numerical Methods in Fluids. 47, 3, p. 253-269 17 p.

Research output: Contribution to journalArticle

19 Scopus citations

Fully coupled fluid-structural interactions using an efficient high resolution upwind scheme

Chen, X. Y. & Zha, G. C., Nov 2005, In : Journal of Fluids and Structures. 20, 8, p. 1105-1125 21 p.

Research output: Contribution to journalArticle

55 Scopus citations

Low-diffusion efficient upwind scheme

Zha, G. C., May 2005, In : AIAA journal. 43, 5, p. 1137-1140 4 p.

Research output: Contribution to journalArticle

24 Scopus citations
2004

Boundary-layer loss mechanism and assessment of wall functions for turbulence modeling

Zha, G. C., Nov 2004, In : AIAA journal. 42, 11, p. 2387-2390 4 p.

Research output: Contribution to journalArticle

2 Scopus citations

Calculation of Transonic Internal Flows Using an Efficient High-Resolution Upwind Scheme

Zha, G. C. & Hu, Z., Feb 2004, In : AIAA journal. 42, 2, p. 205-214 10 p.

Research output: Contribution to journalArticle

36 Scopus citations
1999

Numerical tests of upwind scheme performance for entropy condition

Zha, G. C., Aug 1999, In : AIAA journal. 37, 8, p. 1005-1007 3 p.

Research output: Contribution to journalArticle

14 Scopus citations
1998

Investigations of high-speed civil transport inlet unstart at angle of attack

Zha, G. C., Knight, D. & Smith, D., Jan 1 1998, In : Journal of Aircraft. 35, 6, p. 851-856 6 p.

Research output: Contribution to journalArticle

24 Scopus citations

Numerical simulation of high-speed civil transport inlet operability with angle of attack

Zha, G. C., Knight, D., Smith, D. & Haas, M., Jul 1998, In : AIAA journal. 36, 7, p. 1223-1229 7 p.

Research output: Contribution to journalArticle

31 Scopus citations
1997

High-performance supersonic missile inlet design using automated optimization

Zha, G. C., Smith, D., Schwabacher, M., Rasheed, K., Gelsey, A., Knight, D. & Haas, M., Jan 1 1997, In : Journal of Aircraft. 34, 6, p. 697-705 9 p.

Research output: Contribution to journalArticle

35 Scopus citations
1996

Numerical study of three-dimensional flows using unfactored upwind-relaxation sweeping algorithm

Zha, G. C. & Bilgen, E., May 1996, In : Journal of Computational Physics. 125, 2, p. 425-433 9 p.

Research output: Contribution to journalArticle

25 Scopus citations

Three-dimensional shock/boundary-layer interaction using reynolds stress equation turbulence model

Zha, G. C. & Knight, D., Jul 1996, In : AIAA journal. 34, 7, p. 1313-1320 8 p.

Research output: Contribution to journalArticle

19 Scopus citations
1993

Numerical solutions of Euler equations by using a new flux vector splitting scheme

Zha, G. C. & Bilgen, E., Jul 30 1993, In : International Journal for Numerical Methods in Fluids. 17, 2, p. 115-144 30 p.

Research output: Contribution to journalArticle

78 Scopus citations
1989

An efficient upwind/relaxation algorithm for the Euler and Navier–Stokes equations

Zha, GC. C., Liu, DZ. Z. & Ma, TY. Y., May 1989, In : International Journal for Numerical Methods in Fluids. 9, 5, p. 517-529 13 p.

Research output: Contribution to journalArticle

3 Scopus citations