Chunhua Sheng
Contact Info
Overview
overview
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I earned my Ph.D. degree in Aerospace Engineering from Mississippi State University in 1994. After graduation, I was employed as a Research Engineer, Assistant Research Professor, and Associate Research Professor at NFS/MSU Engineering Research Center for Computational Field Simulation. I joined the faculty in the Department of Mechanical, Industrial, and Manufacturing Engineering at The University of Toledo in 2009. I have taught both undergraduate and graduate courses, and developed a High Performance Computing Laboratory and research program in College of Engineering. My research interests have included development and application of Computational Fluid Dynamics simulations to solve real-world engineering aerodynamic problems.
Publications
selected publications
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Article (Faculty180)
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2020Improving Predictions of Transitional and Separated Flows Using RANS Modeling. Aerospace Science and Technology.
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2018Comparative Study of Yaw and Nacelle Tilt Control Strategies for a Two-bladed Downwind Wind Turbine. Fluid Mechanics Research International Journal. Vol. 2.
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2018Comparative Study of Yaw and Nacelle Tilt Control Strategies for a Two-bladed Downwind Wind Turbine. Fluid Mechanics Research International Journal. Vol. 2:https://medcraveonline.com/FMRIJ/FMRIJ.
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2018Computational Investigation of a Full-Scale Proprotor Hover Performance and Flow Transition. Journal of Aircraft. 55:23-37.
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2018Computational Investigation of a Full-Scale Proprotor Hover Performance and Flow Transition. Journal of Aircraft. Vol. 55:122-132.
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2017
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2017Numerical Investigations of Fan-In-Wing Aerodynamic Performance with Active Flow Control. Journal of Aircraft. 54:2317-2329.
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2017Numerical Investigations of Fan-In-Wing Aerodynamic Performance with Active Flow Control. Journal of Aircraft.
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2016Analysis of swirling flow effects on the characteristics of unsteady hot-streak migration. Chinese Journal of Aeronautics. 29:1469.
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2016Improved Rotor Hover Predictions Using Advanced Turbulence Modeling. Journal of Aircraft. 53:1549-1560.
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2014Computational Aerodynamic Analysis of Offshore Upwind and Downwind Turbines. Journal of Aerodynamics. 2014.
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2013Study of Turbine Conjugate Heat Transfer Simulation Based on Unstructured Grids. Gas Turbine Experiment and Research. 2:010.
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2010Aerodynamic analysis of a spinning missile using a high-order unstructured-grid scheme. Journal of Spacecraft and Rockets. 47:81.
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2009Implicit algorithms for viscous flow simulation at arbitrary Mach number [J]. Acta Aerodynamica Sinica. 5:011.
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1999Multiblock approach for calculating incompressible fluid flows on unstructured grids. AIAA journal. 37:169.
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1988The experimental investigation of the formation and decay of vortices generated by a jet in a crossflow. ACTA Aerodynamica Sinica. 6:104-109.
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Article (Web of Science)
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2020Improving predictions of transitional and separated flows using RANS modeling. AEROSPACE SCIENCE AND TECHNOLOGY. 106.Full Text via DOI: 10.1016/j.ast.2020.106067
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2020A new method towards high-order weno schemes on structured and unstructured grids. COMPUTERS & FLUIDS. 200.Full Text via DOI: 10.1016/j.compfluid.2020.104453
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2018Computational Investigation of a Full-Scale Proprotor Hover Performance and Flow Transition. JOURNAL OF AIRCRAFT. 55:122-132.Full Text via DOI: 10.2514/1.C034015
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2018Role of Transition Modeling in Rotor Hover Predictions. JOURNAL OF AIRCRAFT. 55:23-37.Full Text via DOI: 10.2514/1.C034137
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2018Computational Investigation of a Full-Scale Proprotor Hover Performance and Flow Transition. JOURNAL OF AIRCRAFT. 55:122-132.Full Text via DOI: 10.2514/1.c034015
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2018Role of Transition Modeling in Rotor Hover Predictions. JOURNAL OF AIRCRAFT. 55:23-37.Full Text via DOI: 10.2514/1.c034137
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2017Numerical Investigations of Fan-in-Wing Aerodynamic Performance with Active Flow Control. JOURNAL OF AIRCRAFT. 54:2317-2329.Full Text via DOI: 10.2514/1.C034134
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2017Numerical Investigations of Fan-in-Wing Aerodynamic Performance with Active Flow Control. JOURNAL OF AIRCRAFT. 54:2317-2329.Full Text via DOI: 10.2514/1.c034134
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2016Improved Rotor Hover Predictions Using Advanced Turbulence Modeling. JOURNAL OF AIRCRAFT. 53:1549-1560.Full Text via DOI: 10.2514/1.C033512
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2016Improved Rotor Hover Predictions Using Advanced Turbulence Modeling. JOURNAL OF AIRCRAFT. 53:1549-1560.Full Text via DOI: 10.2514/1.c033512
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2013Efficient Mesh Deformation Using Radial Basis Functions on Unstructured Meshes. AIAA JOURNAL. 51:707-720.Full Text via DOI: 10.2514/1.J052126
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2013Efficient Mesh Deformation Using Radial Basis Functions on Unstructured Meshes. AIAA JOURNAL. 51:707-720.Full Text via DOI: 10.2514/1.j052126
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2011A Preconditioned Method for Rotating Flows at Arbitrary Mach Number. MODELLING AND SIMULATION IN ENGINEERING. 2011:1-17.Full Text via DOI: 10.1155/2011/537464
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2010Aerodynamic Analysis of a Spinning Missile Using a High-Order Unstructured-Grid Scheme. JOURNAL OF SPACECRAFT AND ROCKETS. 47:81-89.Full Text via DOI: 10.2514/1.42988
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2009Computational Simulation and Analysis of Bell Boeing Quad Tiltrotor Aero Interaction. Journal of the American Helicopter Society. 54:042002.Full Text via DOI: 10.4050/jahs.54.042002
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2008Unsteady Simulations of Bell-Agusta 609 Rotor Undergoing Higher Harmonic Oscillation. JOURNAL OF AIRCRAFT. 45:971-980.Full Text via DOI: 10.2514/1.32877
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Book (Faculty180)
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2017Advances in Transitional Flow Modelling. Springer Nature.
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Chapter (Faculty180)
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2010A Preconditioned Arbitrary Mach Number Scheme Applied to Rotating Machinery. Computational Fluid Dynamics. InTech.
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Other Scholarly Work (Faculty180)
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2006HI-ARMS Technical Objective A-TC-3: Unstructured Solver Performance Evaluation. Defense Technical Information Center .
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1996Multigrid computations of 3-D incompressible internal and external viscous rotating flows. NASA Technical Report.
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1994Development of a multiblock multigrid algorithm for the three-dimensional incompressible Navier-Stokes equations. Ph.D. Dissertation, Department of Aerospace Engineering, Mississippi State University.
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Patent (Faculty180)
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Proceedings (Faculty180)
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Proceedings Paper (Web of Science)
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2017AEROMECHANICAL ANALYSIS OF TWO-BLADED DOWNWIND TURBINE USING A NACELLE TILT CONTROL. PROCEEDINGS OF THE ASME FLUIDS ENGINEERING DIVISION SUMMER MEETING, 2017, VOL 1B.
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2017COMPUTATIONAL AERODYNAMIC ANALYSIS OF DOWNWIND TURBINE USING A NEW TILT CONTROL CONCEPT. PROCEEDINGS OF THE ASME FLUIDS ENGINEERING DIVISION SUMMER MEETING, 2017, VOL 1B.
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Contact
full name
- Chunhua Sheng
visualizations
Cumulative publications in Scholars@UToledo