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Contact Us

Main Campus
4004 Nitschke Hall MS 312
1650 N. Westwood
Toledo, OH 43606-3390
Phone: (419) 530-8210
Fax: (419) 530-8206

Chunhua Sheng, Ph.D.

chengAssociate Professor, Mechanical Engineering
Director, High Performance Computing Laboratory 

The University of Toledo
2801 W. Bancroft St., MS 312
Toledo, OH 43606-3390

Office: NI 4064
Phone: (419) 530-8248
Fax: (419) 530-8206
Email: Chunhua.Sheng@UToledo.Edu

SELECTED PUBLICATIONS

  • Gaffey, T., Zhang, C., Quackenbush, T., Sheng, C. and Saberi, H., “Aeromechanics of the Coaxial Compound Helicopter,” AIAA-2015-1411, AIAA 2015 SciTech Conferences, 5-9 January 2015, Kissimmee, Florida.
  • Sheng, C., Wang, J. and Zhao, Q., “S-76 Rotor Hover Predictions Using Advanced Turbulence Models,” AIAA-2015-1715, AIAA 2015 SciTech Conferences, 5-9 January 2015, Kissimmee, Florida.
  • Zhao, Q., Sheng, C. and Bi, N., “Numerical Investigations of Ducted Fan Hover Performance for Fan-In-Wing Applications,” AIAA-2015-1935, AIAA 2015 SciTech Conferences, 5-9 January 2015, Kissimmee, Florida.
  • Wang, J. and Sheng, C., “Comparison of a Local Correlation-Based Transition Model Coupled with SA and SST Turbulence Models,” AIAA-2015-0587, AIAA 2015 SciTech Conferences, 5-9 January 2015, Kissimmee, Florida.
  • Wang, J. and Sheng, C., “Validations of a Local Correlation-Based Transition Model in an Unstructured Grid CFD Solver,” AIAA 2014 Aviation Conference, 16-20 June 2014, Hyatt Atlanta, Atlanta, Georgia
  • Ickes, J., Wang, J., Zhao, Q., and Sheng, C., “Coupled CFD/CSD Simulations of UH60A Rotor at High Thrust,” AIAA 2014 Aviation Conference, 16-20 June 2014, Hyatt Atlanta, Atlanta, Georgia
  • Sheng, C., “Predictions of JVX Rotor Performance in Hover and Airplane Mode Using High-Fidelity Unstructured Grid CFD Solver,” Proceedings of the American Helicopter Society 70th Annual Forum, Montreal, Canada, 20-22 May 2014
  • Zhao, Q., Ickes, J., Sheng, C., and Afjeh, A., “Numerical Investigations of Upwind and Downwind NREL 5MW Reference Wind Turbines Using CFD and CSD,” Proceedings of the American Helicopter Society 70th Annual Forum, Montreal, Canada, 20-22 May 2014
  • Sheng, C., Zhao, Q., and Wang, J., “S-76 Main Rotor Hover Predictions Using U2NCLE Solver,” Invited Presentation at 2014 SciTech Conferences, January 13-17, 2014, National Harbor, Maryland
  • Ickes, J., Wang, J., Zhao, Q., and Sheng, C., “Coupled CFD/CSD Simulations of Helicopter Rotor with a Free Wake Model,” AIAA 2014 SciTech Conferences, January 13-17, 2014, National Harbor, Maryland
  • Sheng, C., Ickes, J., Wang, J., and Zhao, Q., “CFD/CSD Coupled Simulations for a Helicopter Rotor in Forward and Maneuvering Flight,” 31st AIAA Applied Aerodynamics Conference, 24-27 June 2013, San Diego, California
  • Sheng, C., Ickes, J., Zhao, Q., and Narramore, J., “A Loosely Coupled CFD/CSD Simulation of a Helicopter Rotor in Forward Flight,” 69th AHS Annual Forum and Technology Display, 21-23 May 2013, Phoenix, Arizona
  • Sheng, C., and Allen, C., “Efficient Mesh Deformation Using Radial Basis Functions on Unstructured Meshes,” AIAA Journal, March 2013, Vol. 51, No. 3 : pp. 707-720, (doi: 10.2514/1.J052126)
  • Wang, J., Ge, N., Sheng, C., “Implicit Algorithm for Viscous Compressible Flow on Unstructured Grids,” Journal of Aerospace Power, ISSN: 1000-8055, Vol. 27, June, 2012, pp. 1312-1319
  • Zhao, Q., and Sheng, C., “Evaluation of Higher Order Improvement of Unstructured Schemes for Helicopter Rotor Simulations,” AIAA-2012-2901, 30th AIAA Applied Aerodynamics Conference, 25-28 June 2012, New Orleans, Louisiana
  • Sheng, C., and Allen, C., “Efficient Mesh Deformation Using Radial Basis Functions on Unstructured Meshes,” AIAA-2012-2685, 42nd AIAA Fluid Dynamics Conference and Exhibit, 25-28 June 2012, New Orleans, Louisiana
  • Zhao, Q., and Sheng, Q., “Improvements of High-Order Unstructured Grid Schemes Through RBF Interpolation-II,” 50th AIAA Aerospace Sciences Meeting Including the New Horizons Forum and Aerospace Exposition, 2-5 January 2012, Nashville, Tennessee
  • Sheng, C., “A Preconditioned Method for Rotating Flows at Arbitrary Mach Number,” Modeling and Simulation in Engineering, ISSN: 1687-5591, Vol. 2011, January 2011, Article ID 537464, 17 pages, doi:10.1155/2011/537464
  • Su, X., Sheng, C., Allen, C., “An Efficient Mesh Deformation Approach Based on Radial Basis Functions in Unstructured Flow Solver,” Proceedings of 20th AIAA Computational Fluid Dynamics Conference, June 7-30, 2011, Honolulu, Hawaii
  • Zhao, Q. and Sheng, C., “Improvements of High-Order Unstructured Grid Schemes Through RBF Interpolation,” Proceedings of 20th AIAA Computational Fluid Dynamics Conference, June 7-30, 2011, Honolulu, Hawaii
  • Sheng, C., Su, X., Zhao, Q., Bridgeman, J., and Narramore, J., “A Hybrid CFD Method for Helicopter Rotors with Mesh Deformation,” Proceedings of the American Helicopter Society Specialists’ Meeting Next Generation Vertical Lift Technologies, February 23-25, 2011, Fort Worth, Texas
  • Sheng, C., Zhao, Q., Rajmohan, N., Sankar, L., Bridgeman, J., and Narramore, J., “An Unstructured Hybrid CFD Approach for Computing Rotor Wake Flows,” AIAA-2011-1124, 49th AIAA Aerospace Sciences Meeting, 3-6 January, 2011, Orlando, Florida
  • Sheng, C. and Zhao Q. “Application and Validation of High-Order Unstructured Grid Schemes to Vortex-Dominant Flows,” Proceedings of the American Helicopter Society 66th Annual Forum, 11-13 May 2010, Phoenix, Arizona
  • Sheng, C., Wang, X., and Zhao, Q., “Aerodynamic Analysis of a Spinning Missile Using a High Order Unstructured Grid Scheme,” Journal of Spacecraft and Rockets, ISSN: 0022-4650, Vol. 47, No. 1, Jan-Feb 2010, pp. 81-89
  • Yan, M., Su, X., Wei, R., and Sheng, C., “Predicting Transitional Flows Using a New Two-Equation Low-Reynolds-Number Turbulence Model with Transition Sensitivity,” Journal of Aerospace Power, ISSN: 1000-8055, Vol. 24, No. 12, Dec. 2009, pp. 1-6
  • Sheng, C. and Narramore, J., “Computational Simulation and Analysis of Bell Quad Tilt Rotor Aero Interaction Using a Navier-Stokes Flow Solver,” Journal of the American Helicopter Society, ISSN: 0002-8711, DOI: 10.4050/JAHS.54.042000, Vol. 54, No. 4, October, 2009, pp. 042002-1~042002-15
  • Sheng, C., and Wang, X., “Aerodynamic Analysis of a Spinning Missile with Dithering Canards using a Higher Order Unstructured Grid Scheme,” AIAA-2009-1090, 47th AIAA Aerospace Sciences Meeting, 5-8 January 2009, Orlando, Florida 
Last Updated: 4/11/17