Research Interests
 Computational Fluid Dynamics, Aircraft design, Hypersonic aerodynamics                                                                               
 
Education
Bachelor,1999.9-2003.7, Nanjing University of Aeronautics and Astronautics                                                                                       
Doctor,2003.9-2008.12, Nanjing University of Aeronautics and Astronautics                                                                                    
                                                                                  
 
Representative Publications
[1]You, Y.*, (2011). An Overview of the Advantages and Concerns of Hypersonic Inward Turning Inlets. AIAA Publication, 10.2514/6.2011-2269.
[2]You, Y.*, Ludeke, H., Hannemann, K., (2011). Numerical Study Of Compressible Mixing Layers With The DLR TAU Code. Proceedings of European Symposium on Aerothermodynamics, 692-698.
[3]You, Y.*, Luedeke, H., Hannemann, K., (2012). On the Flow Physics of a Low Momentum Flux Ratio Jet in a Supersonic Turbulent Crossflow. Europhysics Letters, 97(2), 24001-24006.
[4]You, Y.*, Buanga, B., Hannemann, V., Luedeke, H., (2012). Evaluation of Turbulence Models in Predicting Hypersonic and Subsonic Base Flows using Grid Adaptation Techniques. Chinese Journal of Aeronautics, 25(3), 325-334.
[5]You, Y.*, Luedeke, H., Eggers, T., Hannemann, K., (2012). Application of the y-Reot Transition Model in High Speed Flows. AIAA Publication, 10.2514/6.2012-5972.
[6]You Y.*, Kai O., Luedeke H., Hannemann, V., (2012). Numerical Study of the Subsonic Base Flow with a Side Support. Progress in Hybrid RANS-LES Modelling: Notes on Numerical Fluid Mechanics & Multidisciplinary Design. Springer Berlin Heidelberg, 2012:427-437.
[7]You Y.*, Liang D.,(2012). A Non-linear Eddy-Viscosity View of Shock Wave/Boundary Layer Interaction Flow Simulation. 28th International Symposium on Shock Waves. Springer Berlin Heidelberg, 465-470.
[8]You, Y.*, Luedeke, H., Hannemann, K., (2013). Injection and Mixing in a Scramjet Combustor: DES and RANS Studies. Proceedings of the Combustion Institute, 34(2), 2083-2092.
[9]Li, Y., An, P., Chen R., You, Y.*, (2015). Integration Methodology for Waverider-Derived Hypersonic Inlet and Vehicle Forebody. AIAA Publication, 10.2514/6.2014-3229.
Teng, J., You, Y*. Pan, C., (2015). Flow Distortion Generation and Management of an Axisymmetric Ramjet Engine, AIAA Publication, 10.2514/ 6. 2015-3592.
[10]Li, Y., Han, W., Teng, J., You, Y.*, (2015). An Innovative Integration Concept for Forebody and Two-Dimensional Hypersonic Inlet with Controllable Wall Pressure Distribution, AIAA Publication, 10.2514/ 6. 2015-3592.