| Year |
Citation |
Score |
| 2020 |
Zhong D, Sheng C. A New Method Towards High-Order WENO Schemes on Structured and Unstructured Grids Computers & Fluids. 200: 104453. DOI: 10.1016/J.Compfluid.2020.104453 |
0.351 |
|
| 2017 |
Sheng C, Zhao Q, Hill M. Computational Investigation of a Full-Scale Proprotor Hover Performance and Flow Transition Journal of Aircraft. 55: 122-132. DOI: 10.2514/1.C034015 |
0.574 |
|
| 2016 |
Sheng C, Zhao Q. Numerical investigations of fan-in-wing aerodynamic performance with active flow control 34th Aiaa Applied Aerodynamics Conference. DOI: 10.2514/1.C034134 |
0.584 |
|
| 2016 |
Sheng C, Wang J, Zhao Q. Improved Rotor Hover Predictions Using Advanced Turbulence Modeling Journal of Aircraft. 53: 1549-1560. DOI: 10.2514/1.C033512 |
0.569 |
|
| 2016 |
Wang J, Ge N, Sheng C. Analysis of swirling flow effects on the characteristics of unsteady hot-streak migration Chinese Journal of Aeronautics. 29: 1469-1476. DOI: 10.1016/J.Cja.2016.09.001 |
0.43 |
|
| 2015 |
Sheng C, Zhao Q, Bi NP. Numerical investigations of ducted fan hover performance for fan-in-wing applications 53rd Aiaa Aerospace Sciences Meeting. DOI: 10.2514/6.2015-1935 |
0.35 |
|
| 2015 |
Sheng C, Wang J, Zhao Q. S-76 rotor hover predictions using advanced turbulence models 53rd Aiaa Aerospace Sciences Meeting. DOI: 10.2514/6.2015-1715 |
0.388 |
|
| 2015 |
Wang J, Sheng C. A comparison of a local correlation-based transition model coupled with SA and SST turbulence models 53rd Aiaa Aerospace Sciences Meeting. DOI: 10.2514/6.2015-0587 |
0.303 |
|
| 2015 |
Zhao Q, Sheng C. Numerical investigation and validation of open fan hover performance 33rd Aiaa Applied Aerodynamics Conference. |
0.345 |
|
| 2014 |
Wang J, Sheng C. Validations of a local correlation-based transition model using an unstructured grid CFD solver Aiaa Aviation 2014 -7th Aiaa Theoretical Fluid Mechanics Conference. |
0.316 |
|
| 2014 |
Sheng C. Predictions of JVX rotor performance in hover and airplane mode using high-fidelity unstructured grid CFD solver Annual Forum Proceedings - Ahs International. 1: 382-396. |
0.371 |
|
| 2014 |
Sheng C, Zhao Q, Wang J. S-76 rotor hover prediction using U2NCLE Solver 52nd Aiaa Aerospace Sciences Meeting - Aiaa Science and Technology Forum and Exposition, Scitech 2014. |
0.327 |
|
| 2014 |
Sheng C, Zhao Q, Wang J. S-76 rotor hover prediction using U<sup>2</sup>NCLE solver 52nd Aerospace Sciences Meeting. |
0.31 |
|
| 2013 |
Sheng C, Allen CB. Efficient mesh deformation using radial basis functions on unstructured meshes Aiaa Journal. 51: 707-720. DOI: 10.2514/1.J052126 |
0.34 |
|
| 2012 |
Zhao Q, Sheng C. Improvements of high order unstructured grid schemes through RBF interpolation - II 50th Aiaa Aerospace Sciences Meeting Including the New Horizons Forum and Aerospace Exposition. DOI: 10.2514/6.2012-727 |
0.397 |
|
| 2012 |
Zhao Q, Sheng C. Evaluation of higher order improvement of unstructured schemes for helicopter rotor simulations 30th Aiaa Applied Aerodynamics Conference 2012. 967-982. |
0.346 |
|
| 2011 |
Sheng C. A preconditioned method for rotating flows at arbitrary Mach number Modelling and Simulation in Engineering. 2011. DOI: 10.1155/2011/537464 |
0.482 |
|
| 2011 |
Zhao Q, Sheng C. Improvements of high-order unstructured grid schemes through RBF interpolation 20th Aiaa Computational Fluid Dynamics Conference 2011. |
0.314 |
|
| 2010 |
Sheng C, Wang X, Zhao Q. Aerodynamic analysis of a spinning missile using a high-order unstructured-grid scheme Journal of Spacecraft and Rockets. 47: 81-89. DOI: 10.2514/1.42988 |
0.569 |
|
| 2010 |
Sheng C, Zhao Q. Application and validation of high-order unstructured grid schemes to vortex-dominant flows Annual Forum Proceedings - Ahs International. 1: 244-270. |
0.409 |
|
| 2009 |
Sheng C, Narramore JC. Computational simulation and analysis of bell boeing quad tiltrotor aero interaction Journal of the American Helicopter Society. 54. DOI: 10.4050/Jahs.54.042002 |
0.411 |
|
| 2009 |
Sheng C, Wang X. Aerodynamic analysis of a spinning missile with dithering canards using a high order unstructured grid scheme 47th Aiaa Aerospace Sciences Meeting Including the New Horizons Forum and Aerospace Exposition. |
0.383 |
|
| 2008 |
Sheng C, Narramore JC. Computational simulation and analysis of bell boeing quad tiltrotor aero interaction using a Navier-stoke flow solver Annual Forum Proceedings - Ahs International. 1: 45-58. |
0.339 |
|
| 2007 |
Sheng C, Narramore JC. Unsteady simulations of bell-agusta 609 rotor undergoing higher harmonic oscillation Collection of Technical Papers - Aiaa Applied Aerodynamics Conference. 1: 524-536. DOI: 10.2514/1.32877 |
0.44 |
|
| 2006 |
Sheng C, Wang X. A global preconditioning method for low mach number viscous flows in rotating machinery Proceedings of the Asme Turbo Expo. 6: 1555-1564. DOI: 10.1115/GT2006-91189 |
0.378 |
|
| 2005 |
Wang X, Sheng C, Chen JP. Numerical study of preconditioned algorithm for rotational flows 17th Aiaa Computational Fluid Dynamics Conference. |
0.418 |
|
| 2005 |
Sheng C, Xue Q. Aerothermal analysis of turbine blades using an unstructured flow solver - U2NCLE 38th Aiaa Thermophysics Conference. |
0.354 |
|
| 2004 |
Sheng C, Remotigue M. Numerical simulations of rotor 35 with and without tip injection using an arbitrary mach number flow solver Aiaa Paper. 50-59. |
0.372 |
|
| 2004 |
Sheng C. Full annulus simulation of a high-speed centrifugal compressor using an unstructured rans flow solver Proceedings of the Asme Turbo Expo 2004. 5: 1601-1611. |
0.357 |
|
| 2003 |
Sheng C, Wang X. Characteristic variable boundary conditions for arbitrary mach number algorithm in rotating frame 16th Aiaa Computational Fluid Dynamics Conference. |
0.379 |
|
| 1999 |
Sheng C, Whitfield DL, Anderson WK. Multiblock Approach for Calculating Incompressible Fluid Flows on Unstructured Grids Aiaa Journal. 37: 169-176. DOI: 10.2514/2.710 |
0.384 |
|
| 1995 |
Sheng C, Taylor LK, Whitefield DL. Multigrid algorithm for three-dimensional incompressible high-Reynolds number turbulent flows Aiaa Journal. 33: 2073-2079. DOI: 10.2514/3.12949 |
0.445 |
|
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