GeCheng Zha

Professor

  • 2075 Citations
1989 …2020

Research output per year

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Research Output

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Conference contribution

3D simulation of a transonic wing flutter using an efficient high resolution upwind scheme

Chen, X., Zha, G. C. & Yang, M. T., 2006, Collection of Technical Papers - 36th AIAA Fluid Dynamics Conference. American Institute of Aeronautics and Astronautics Inc., p. 849-866 18 p. (Collection of Technical Papers - 36th AIAA Fluid Dynamics Conference; vol. 2).

Research output: Chapter in Book/Report/Conference proceedingConference contribution

3D steady hypersonic laminar MHD flow using high order weno schemes

Lee, J., Huerta, M. A. & Zha, G., Jan 1 2009, 40th AIAA Plasmadynamics and Lasers Conference. American Institute of Aeronautics and Astronautics Inc., 2009-3913. (40th AIAA Plasmadynamics and Lasers Conference).

Research output: Chapter in Book/Report/Conference proceedingConference contribution

1 Scopus citations

A constrained-transport E-CUSP scheme for ideal magnetohydrodynamic equations

Shen, Y., Zha, G. & Huerta, M. A., Dec 1 2011, 42nd AIAA Plasmadynamics and Lasers Conference. (42nd AIAA Plasmadynamics and Lasers Conference).

Research output: Chapter in Book/Report/Conference proceedingConference contribution

A constrained-transport E-CUSP scheme for ideal magnetohydrodynamic equations

Shen, Y., Zha, G. & Huerta, M. A., 2011, 42nd AIAA Plasmadynamics and Lasers Conference. American Institute of Aeronautics and Astronautics Inc., (42nd AIAA Plasmadynamics and Lasers Conference).

Research output: Chapter in Book/Report/Conference proceedingConference contribution

A general sub-domain boundary mapping procedure for structured grid CFD parallel computation

Wang, B. & Zha, G. C., 2007, Collection of Technical Papers - 25th AIAA Applied Aerodynamics Conference, 2007. American Institute of Aeronautics and Astronautics Inc., p. 1774-1788 15 p. (Collection of Technical Papers - AIAA Applied Aerodynamics Conference; vol. 3).

Research output: Chapter in Book/Report/Conference proceedingConference contribution

1 Scopus citations

A high efficiency low noise vtol/estol concept using coflow jet airfoil

Zha, G., Ren, Y., Gan, J. & Espinal, D., Jan 1 2019, AIAA Propulsion and Energy Forum and Exposition, 2019. American Institute of Aeronautics and Astronautics Inc, AIAA, (AIAA Propulsion and Energy Forum and Exposition, 2019).

Research output: Chapter in Book/Report/Conference proceedingConference contribution

A hybrid Cartesian-body fitted grid approach for simulation of flows in complex geometries

Chen, X. & Zha, G. C., 2009, 19th AIAA Computational Fluid Dynamics Conference. 2009-3880. (19th AIAA Computational Fluid Dynamics Conference).

Research output: Chapter in Book/Report/Conference proceedingConference contribution

2 Scopus citations

Aircraft control surfaces using co-flow jet active flow control airfoil

Zhang, J., Xu, K., Yang, Y., Yan, R., Patel, P. & Zha, G., 2018, 2018 Applied Aerodynamics Conference. American Institute of Aeronautics and Astronautics Inc, AIAA, AIAA 2018-3067. (2018 Applied Aerodynamics Conference).

Research output: Chapter in Book/Report/Conference proceedingConference contribution

4 Scopus citations

A low diffusion E-CUSP upwind scheme for transonic flows

Zha, G. C., 2004, 34th AIAA Fluid Dynamics Conference and Exhibit. American Institute of Aeronautics and Astronautics Inc., (34th AIAA Fluid Dynamics Conference and Exhibit).

Research output: Chapter in Book/Report/Conference proceedingConference contribution

9 Scopus citations

Analysis of a low boom supersonic flying wing preliminary design

Gan, J. & Zha, G., Jan 1 2015, 53rd AIAA Aerospace Sciences Meeting. American Institute of Aeronautics and Astronautics Inc, AIAA, (53rd AIAA Aerospace Sciences Meeting).

Research output: Chapter in Book/Report/Conference proceedingConference contribution

1 Scopus citations

Analysis of jet effects on co-flow jet airfoil performance with integrated propulsion system

Zha, G. C. & Gao, W., 2006, Collection of Technical Papers - 44th AIAA Aerospace Sciences Meeting. American Institute of Aeronautics and Astronautics Inc., p. 1273-1291 19 p. (Collection of Technical Papers - 44th AIAA Aerospace Sciences Meeting; vol. 2).

Research output: Chapter in Book/Report/Conference proceedingConference contribution

11 Scopus citations

A novel airfoil circulation augment flow control method using co-flow jet

Zha, G. C. & Paxton, C., 2004, 2nd AIAA Flow Control Conference. American Institute of Aeronautics and Astronautics Inc., (2nd AIAA Flow Control Conference).

Research output: Chapter in Book/Report/Conference proceedingConference contribution

23 Scopus citations

Application of co-flow jet concept on thin airfoil at high angle of attack

Rachman, A., Tsai, H. M. & Zha, G. C., Jan 1 2006, Collection of Technical Papers - 3rd AIAA Flow Control Conference. American Institute of Aeronautics and Astronautics Inc., p. 125-146 22 p. (Collection of Technical Papers - 3rd AIAA Flow Control Conference; vol. 1).

Research output: Chapter in Book/Report/Conference proceedingConference contribution

1 Scopus citations

Application of low diffusion E-CUSP scheme with high order WENO scheme for chemical reacting flows

Shen, Y. & Zha, G., 2010, 40th AIAA Fluid Dynamics Conference. American Institute of Aeronautics and Astronautics Inc., 2010-4995. (40th AIAA Fluid Dynamics Conference; vol. 1).

Research output: Chapter in Book/Report/Conference proceedingConference contribution

1 Scopus citations

A robust seventh-order WENO scheme and its applications

Shen, Y. & Zha, G., Dec 1 2008, 46th AIAA Aerospace Sciences Meeting and Exhibit. 2008-0757. (46th AIAA Aerospace Sciences Meeting and Exhibit).

Research output: Chapter in Book/Report/Conference proceedingConference contribution

15 Scopus citations

Boundary layer loss mechanism and justification of wall functions for turbulence modeling

Zha, G., Jul 1 2004, AIAA Paper. p. 7054-7067 14 p.

Research output: Chapter in Book/Report/Conference proceedingConference contribution

1 Scopus citations

Calculation of transonic flows using WENO method with a low diffusion E-CUSP upwind scheme

Zha, G. C., Shen, Y. & Wang, B., 2008, 46th AIAA Aerospace Sciences Meeting and Exhibit. American Institute of Aeronautics and Astronautics Inc., 2008-0745. (46th AIAA Aerospace Sciences Meeting and Exhibit).

Research output: Chapter in Book/Report/Conference proceedingConference contribution

27 Scopus citations

Calculation of transonic internal flows using an efficient high resolution upwind scheme

Zha, G. & Hu, Z., Jul 1 2004, AIAA Paper. p. 6853-6866 14 p.

Research output: Chapter in Book/Report/Conference proceedingConference contribution

1 Scopus citations

Characterization of RAE 2822 transonic airfoil in FSU polysonic wind tunnel facility

Kumar, R., Richardson, R., Gustavsson, J., Cattafesta, L., Kumar, R., Liu, Z. & Zha, G., Jan 1 2018, AIAA Aerospace Sciences Meeting. 210059 ed. American Institute of Aeronautics and Astronautics Inc, AIAA

Research output: Chapter in Book/Report/Conference proceedingConference contribution

Co-flow jet airfoil trade study part I: Energy consumption and aerodynamic efficiency

Lefebvre, A. & Zha, G. C., Jan 1 2014, 32nd AIAA Applied Aerodynamics Conference. American Institute of Aeronautics and Astronautics Inc., (32nd AIAA Applied Aerodynamics Conference).

Research output: Chapter in Book/Report/Conference proceedingConference contribution

11 Scopus citations

Co-flow jet airfoil trade study part II: Moment and drag

Lefebvre, A. & Zha, G. C., Jan 1 2014, 32nd AIAA Applied Aerodynamics Conference. American Institute of Aeronautics and Astronautics Inc., (32nd AIAA Applied Aerodynamics Conference).

Research output: Chapter in Book/Report/Conference proceedingConference contribution

9 Scopus citations

Comparative study of upwind scheme performance for entropy condition and discontinuities

Zha, G., 1999, 14th Computational Fluid Dynamics Conference. American Institute of Aeronautics and Astronautics Inc, AIAA, p. 800-813 14 p.

Research output: Chapter in Book/Report/Conference proceedingConference contribution

2 Scopus citations

Comparison of a low diffusion E-CUSP and the Roe scheme for RANS calculation

Wang, B. & Zha, G. C., Dec 1 2008, 46th AIAA Aerospace Sciences Meeting and Exhibit. 2008-0569. (46th AIAA Aerospace Sciences Meeting and Exhibit).

Research output: Chapter in Book/Report/Conference proceedingConference contribution

13 Scopus citations

Comparison of drag prediction using RANS models and DDES for the DLR-F6 configuration using high order schemes

Gan, J., Shen, Y. & Zha, G., 2016, 54th AIAA Aerospace Sciences Meeting. American Institute of Aeronautics and Astronautics Inc, AIAA, (54th AIAA Aerospace Sciences Meeting; vol. 0).

Research output: Chapter in Book/Report/Conference proceedingConference contribution

6 Scopus citations

Comparison of high order schemes for large eddy simulation of circular cylinder flow

Shen, Y. & Zha, G., 2009, 47th AIAA Aerospace Sciences Meeting including the New Horizons Forum and Aerospace Exposition. American Institute of Aeronautics and Astronautics Inc., 2009-0945. (47th AIAA Aerospace Sciences Meeting including the New Horizons Forum and Aerospace Exposition).

Research output: Chapter in Book/Report/Conference proceedingConference contribution

9 Scopus citations

Comparisons of high order hybrid schemes using a parameter-free discontinuity detector

Shen, Y., Zha, G., Yang, G. & Gao, Z., 2012, 42nd AIAA Fluid Dynamics Conference and Exhibit 2012. American Institute of Aeronautics and Astronautics Inc., (42nd AIAA Fluid Dynamics Conference and Exhibit 2012).

Research output: Chapter in Book/Report/Conference proceedingConference contribution

3 Scopus citations

Comparison study of implicit gauss-seidel line iteration method for transonic flows

Shen, Y., Wang, B. & Zha, G., Nov 7 2007, Collection of Technical Papers - 18th AIAA Computational Fluid Dynamics Conference. p. 1580-1593 14 p. (Collection of Technical Papers - 18th AIAA Computational Fluid Dynamics Conference; vol. 2).

Research output: Chapter in Book/Report/Conference proceedingConference contribution

2 Scopus citations

Conceptual design and study of "engineless" airplane using co-flow jet airfoil

Aguirre, J., Wang, B. Y. & Zha, G. C., Jan 1 2007, Collection of Technical Papers - 25th AIAA Applied Aerodynamics Conference, 2007. American Institute of Aeronautics and Astronautics Inc., p. 1884-1901 18 p. (Collection of Technical Papers - AIAA Applied Aerodynamics Conference; vol. 3).

Research output: Chapter in Book/Report/Conference proceedingConference contribution

3 Scopus citations

Conceptual design of a co-flow jet hybrid electric regional airliner

Yang, Y. & Zha, G., Jan 1 2019, AIAA Scitech 2019 Forum. American Institute of Aeronautics and Astronautics Inc, AIAA, (AIAA Scitech 2019 Forum).

Research output: Chapter in Book/Report/Conference proceedingConference contribution

Conceptual design of a personal aerial vehicle using co-flow jet airfoil

Coronado, P. X., Cuffie, B., Saer, D. & Zha, G. C., Jan 1 2007, Collection of Technical Papers - 25th AIAA Applied Aerodynamics Conference, 2007. American Institute of Aeronautics and Astronautics Inc., p. 1902-1917 16 p. (Collection of Technical Papers - AIAA Applied Aerodynamics Conference; vol. 3).

Research output: Chapter in Book/Report/Conference proceedingConference contribution

3 Scopus citations

Delayed detached eddy simulation of 3-D wing flutter with fully coupled fluid-structural interaction

Chen, X., Wang, B. & Zha, G. C., Dec 14 2010, 48th AIAA Aerospace Sciences Meeting Including the New Horizons Forum and Aerospace Exposition. 2010-0053. (48th AIAA Aerospace Sciences Meeting Including the New Horizons Forum and Aerospace Exposition).

Research output: Chapter in Book/Report/Conference proceedingConference contribution

3 Scopus citations

Delayed detached eddy simulation of projectile flows

Gan, J. & Zha, G. C., Jan 1 2015, 33rd AIAA Applied Aerodynamics Conference. American Institute of Aeronautics and Astronautics Inc, AIAA, (33rd AIAA Applied Aerodynamics Conference).

Research output: Chapter in Book/Report/Conference proceedingConference contribution

Delayed detached eddy simulation of rotating stall for a full annulus transonic axial compressor stage

Gan, J., Im, H. S. & Zha, G. C., 2016, Turbomachinery. American Society of Mechanical Engineers (ASME), (Proceedings of the ASME Turbo Expo; vol. 2A-2016).

Research output: Chapter in Book/Report/Conference proceedingConference contribution

2 Scopus citations

Delayed-detached-eddy simulation of shock wave/turbulent boundary layer interaction

Coronado, P. X., Wang, B. & Zha, G. C., Dec 13 2010, 48th AIAA Aerospace Sciences Meeting Including the New Horizons Forum and Aerospace Exposition. 2010-0109. (48th AIAA Aerospace Sciences Meeting Including the New Horizons Forum and Aerospace Exposition).

Research output: Chapter in Book/Report/Conference proceedingConference contribution

9 Scopus citations

Delayed detached eddy simulation of supersonic panel aeroelasticity using fully coupled fluid structure interaction with high order schemes

Gan, J. & Zha, G., 2016, 34th AIAA Applied Aerodynamics Conference. American Institute of Aeronautics and Astronautics Inc, AIAA, (34th AIAA Applied Aerodynamics Conference).

Research output: Chapter in Book/Report/Conference proceedingConference contribution

1 Scopus citations

Design of high specific speed mixed flow micro-compressor for co-flow jet actuators

Xu, K. & Zha, G., Jan 1 2019, Microturbines, Turbochargers, and Small Turbomachines; Steam Turbines. American Society of Mechanical Engineers (ASME), (Proceedings of the ASME Turbo Expo; vol. 8).

Research output: Chapter in Book/Report/Conference proceedingConference contribution

2 Scopus citations

Design of high wing loading compact electric airplane utilizing co-flow jet flow control

Lefebvre, A. & Zha, G., 2015, 53rd AIAA Aerospace Sciences Meeting. American Institute of Aeronautics and Astronautics Inc, AIAA, AIAA 2015-0772

Research output: Chapter in Book/Report/Conference proceedingConference contribution

19 Scopus citations

Design of injection and suction ducts for co-flow jet airfoils with embedded micro-compressors actuator

Ren, Y. & Zha, G., Jan 1 2018, 2018 Flow Control Conference. [publishername] American Institute of Aeronautics and Astronautics Inc, AIAA, AIAA 2018-3062

Research output: Chapter in Book/Report/Conference proceedingConference contribution

1 Scopus citations

Design of injection jet span profile for co-flow jet airfoil

Ren, Y. & Zha, G., Jan 1 2019, AIAA Scitech 2019 Forum. American Institute of Aeronautics and Astronautics Inc, AIAA, (AIAA Scitech 2019 Forum).

Research output: Chapter in Book/Report/Conference proceedingConference contribution

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

Wang, B. & Zha, G. C., 2009, 39th AIAA Fluid Dynamics Conference. American Institute of Aeronautics and Astronautics Inc., 2009-4015. (39th AIAA Fluid Dynamics Conference).

Research output: Chapter in Book/Report/Conference proceedingConference contribution

2 Scopus citations

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

Wang, B. & Zha, G. C., 2009, 47th AIAA Aerospace Sciences Meeting including the New Horizons Forum and Aerospace Exposition. American Institute of Aeronautics and Astronautics Inc., 2009-1507. (47th AIAA Aerospace Sciences Meeting including the New Horizons Forum and Aerospace Exposition).

Research output: Chapter in Book/Report/Conference proceedingConference contribution

4 Scopus citations

Detached eddy simulation of transonic rotor stall flutter using a fully coupled fluid-structure interaction

Hongsik, I. M., Chen, X. & Zha, G., Dec 1 2011, ASME 2011 Turbo Expo: Turbine Technical Conference and Exposition, GT2011. PARTS A AND B ed. p. 1217-1230 14 p. (Proceedings of the ASME Turbo Expo; vol. 6, no. PARTS A AND B).

Research output: Chapter in Book/Report/Conference proceedingConference contribution

10 Scopus citations

Detached Eddy Simulation of unsteady stall flows of a full annulus transonic rotor

Im, H. S., Chen, X. & Zha, G. C., Dec 1 2010, ASME Turbo Expo 2010: Power for Land, Sea, and Air, GT 2010. PARTS A, B, AND C ed. p. 2627-2642 16 p. (Proceedings of the ASME Turbo Expo; vol. 7, no. PARTS A, B, AND C).

Research output: Chapter in Book/Report/Conference proceedingConference contribution

6 Scopus citations

Detached-eddy simulations of a circular cylinder using a low diffusion E-CUSP and high-order WENO scheme

Wang, B., Zha, G. C. & Shen, Y., 2008, 38th AIAA Fluid Dynamics Conference and Exhibit. American Institute of Aeronautics and Astronautics Inc., 2008-3855. (38th AIAA Fluid Dynamics Conference and Exhibit).

Research output: Chapter in Book/Report/Conference proceedingConference contribution

13 Scopus citations

Distortion elimination for serpentine inlet using coflow jet flow control with variation of mach numbers

Xu, K. & Zha, G., 2020, AIAA Propulsion and Energy 2020 Forum. American Institute of Aeronautics and Astronautics Inc, AIAA, p. 1-16 16 p. (AIAA Propulsion and Energy 2020 Forum).

Research output: Chapter in Book/Report/Conference proceedingConference contribution

Effects of rotor tip clearance on tip clearance flow potentially leading to NSV in an axial compressor

Im, H. S. & Zha, G. C., Dec 1 2012, ASME Turbo Expo 2012: Turbine Technical Conference and Exposition, GT 2012. PARTS A AND B ed. p. 1383-1394 12 p. (Proceedings of the ASME Turbo Expo; vol. 7, no. PARTS A AND B).

Research output: Chapter in Book/Report/Conference proceedingConference contribution

7 Scopus citations

Experimental investigation of jet mixing of a co-flow jet airfoil

Dano, B. P. E., Kirk, D. & Zha, G. C., 2010, 5th Flow Control Conference. 2010-4421. (5th Flow Control Conference).

Research output: Chapter in Book/Report/Conference proceedingConference contribution

9 Scopus citations

Experimental investigations of vehicle base drag reduction using passive jet boat-tail flow control

Bartow, W. B., Moreyra, A. C., Hirst, T., Woyczynski, G. H., Lefebvre, A. & Zha, G., Jan 1 2014, SAE Technical Papers. SAE International

Research output: Chapter in Book/Report/Conference proceedingConference contribution

5 Scopus citations

Experimental study of co-flow jet airfoil performance enhancement using discrete jets

Dano, B. P. E., Zha, G. & Castillo, M., Dec 6 2011, 49th AIAA Aerospace Sciences Meeting Including the New Horizons Forum and Aerospace Exposition. AIAA-2011-941

Research output: Chapter in Book/Report/Conference proceedingConference contribution

32 Scopus citations

Full-annulus simulation of non-synchronous blade vibration excitation of an axial compressor

Espinal, D., Im, H. S. & Zha, G. C., Jan 1 2014, 52nd AIAA Aerospace Sciences Meeting - AIAA Science and Technology Forum and Exposition, SciTech 2014. American Institute of Aeronautics and Astronautics Inc., (52nd AIAA Aerospace Sciences Meeting - AIAA Science and Technology Forum and Exposition, SciTech 2014).

Research output: Chapter in Book/Report/Conference proceedingConference contribution

1 Scopus citations