Personal tools
You are here: Home Publications

List of Publications

Books
  1. Shyy, W., Lian, Y., Tang, J., Viieru, D., and Liu, H., Aerodynamics of Low Reynolds Number Flyers, Cambridge University Press, 2008.

Journal Papers

  1. Shyy, W., Lian, Y., Tang, J., Liu, H., Trizila, P., Stanford, B., Bernal, L., Cesnik, C., Friedman, P., and Ifju, P., "Computational Aerodyanmics of Low Reynolds Number Plunging, Pitching and Flexible Wings for MAV Applications," Review Paper, Acta Mech Sin, Vol. 24, pp. 351-373, 2008.
  2. Lian, Y., and Shyy, W., "Laminar-Turbulent Transition of a Low Reynolds Number Rigid or Flexible Airfoil," AIAA Journal, Vol. 47, No. 7, 2007. 
  3. Lian, Y., and Liou, M-S., "Aero-Structural Optimization of a Transonic Compressor Rotor,"
    Journal of Propulsion and Power, Vol. 22, No. 4, 2006, pp. 880-888.
  4. Lian, Y., and Kim, N-H., "Reliability-based Design Optimization of a Transonic Compressor," AIAA Journal, Vol. 44, No. 2, 2006, pp. 368-375.
  5. Lian, Y., and Liou, M-S., "Multi-objective Optimization of a Transonic Compressor Rotor using Evolutionary Algorithm," Journal of Propulsion and Power, Vol. 21, No. 6, 2005, pp. 979-987.
  6. Lian, Y., and Shyy, W.,"Three-Dimensional Fluid-Structure Interactions of a Membrane Wing for Micro Air Vehicle Applications," Journal of Aircraft, Vol. 42, No. 5, 2005, pp. 865-873.
  7. Lian, Y., and Liou, M-S., "Multi-objective Optimization Using Coupled Response Surface Model and Evolutionary Algorithm,'' AIAA Journal, Vol.43, No.6, 2005, pp. 1316-1325.
  8. Lian, Y., and Liou, M-S., "Mining of Data from Evolutionary Algorithms for Improving
    Design Optimization," Computer Modeling in Engineering & Sciences, Vol. 8, No.1, 2005, pp. 61-72.
  9. Lian, Y., Shyy, W., Viieru, D., and Zhang, B. N., "Membrane Wing Aerodynamics for Micro Air Vehicles," Progress in Aerospace Sciences, Vol. 39, 2003, pp. 425-465.
  10. Lian, Y., Steen, J., Trygg-Wilander, M. and Shyy, W., "Low Reynolds Number Turbulent Flows around a Dynamically Shaped Airfoil," Computers and Fluids, Vol. 32, 2003, pp. 287-303.
  11. Lian, Y., Shyy, W., and Haftka,R., "Shape Optimization of a Membrane Wing for Micro Air Vehicles," AIAA Journal, Vol. 42, 2004, pp. 424-426.
  12. Lian, Y., Shyy, W., Ifju, P., and Verron, E., "A Membrane Wing Model for Micro Air Vehicles," AIAA Journal, Vol. 41, 2003, pp. 2492-2494.
  13. Kamakoti, R., Lian, Y., Regisford, S., Kurdila A. and Shyy, W.,"Computational Aeroelasticity Using a Pressure-based Solver," Computer Modeling in Engineering & Sciences, Vol. 3, 2002, pp. 773-790.
  14. Lian, Y. and Xu, K., "A Gas-Kinetic Scheme for Multi-material Flows and Its Application in Chemical Reactions," Journal of Computational Physics, Vol. 163, 2000, pp. 349-375. 
  15. Lian, Y. and Xu, K., "A Gas-Kinetic Scheme for Reactive Flows," Computers and Fluids, Vol. 29, 2000, pp. 725-748.
  16. Lian, Y. and Wang, R., "A Simplified BGK-type Scheme," Chinese Journal of Computational Mechanics, Vol. 16, 1999, pp. 275-282 (in Chinese).
  17. Lian, Y. and Wang, R., "Multiresolution Scheme Based on WENO Schemes," Chinese Journal of Numerical Mathematics and Applications, Vol. 21, 1999, pp. 58-68.
  18. Lian, Y. and Wang, R., "Multiresolution Scheme Based on WENO," Mathematic Numerica Sinica, Vol. 21, 1999, pp. 215-224.
  19. Lian, Y. and Wang, R., "A Comparison of Upwind Schemes Based on the Boltzmann Equation and the Euler Equations," Communications in Nonlinear Science and Simulation, Vol. 2, 1997, pp. 117-120.
  20. Lian, Y. and Wang, R., "An Implicit Kinetic Flux Vector Splitting Scheme," Communications in Nonlinear Science and Simulation, Vol. 2, 1997, pp. 185-190.


Conference Papers

  1. Lian, Y., "Numerical Investigation of Boundary Effects on Flapping Wing Study," AIAA Paper 2009-539 (Download).
  2. Shyy, W., Lian, Y., Tang, J., Liu, H.,Bernal, L., Cesnik, C., and Friedmann, P., "Computational Aerodynamics of Low Reynolds Number Plunging, Pitching and Flexible Wings," Invited AIAA paper.
  3. Lian, Y., Ol., M., and Shyy, W., "Numerical and Experimental Investigation of Reynolds Number Effect on Flapping Airfoil Aerodynamics," AIAA Paper 2008-0652.
  4. Jayaraman, B., Lian, Y., and Shyy, W., "Low-Reynolds Number Flow Control Using Dielectric Barrier Discharge-Based Actuators," AIAA Paper 2007-3974, Miami, FL, June 2007.
  5. Lian, Y., and Shyy, W., "Aerodynamics of Low Reynolds Number Plunging Airfoil under Gusty Environment," AIAA Paper 2007-71, Reno, NV, 2007.
  6. Lian, Y., and Shyy, W., "Laminar-Turbulent Transition of a Low Reynolds Number Rigid or Flexible Airfoil," AIAA Paper 2006-3051, San Francisco, CA, June 2006.
  7. Viieru, D., Tang, J., Lian, Y., Liu, H., and Shyy, W., "Flapping and Flexible Wing Aerodynamics of Low Reynolds Number Flight Vehicles," AIAA Paper 2006-503, Reno, NV, January 2006.
  8. Lian, Y., and Liou, M., "Aero-Structure Optimization of a Transonic Compressor Blade," AIAA Paper 2005-3634, 41st AIAA/ASME/ASE/ASEE Joint Propulsion Conference & Exhibit, Tucson, Arizona, July 10-13, 2005.
  9. Lian, Y., and Kim, N., "Reliability-based Design Optimization of a Transonic Compressor,'' AIAA Paper 2005-4021, 41st AIAA/ASME/ASE/ASEE Joint Propulsion Conference & Exhibit, Tucson, Arizona, July 10-13, 2005.
  10. Lian, Y., and Liou, M., "Multiobjective Optimization of a Transonic Compressor Blade using Evolutionary Algorithm," AIAA Paper 2005-1816, Austin, TX, June 2005.
  11. Lian, Y., and Liou, M., "Multiobjective Optimization Using Coupled Response Surface Model and Evolutionary Algorithm," AIAA Paper 2004-4323, Albany, NY, August 30-September 1, 2004.
  12. Lian, Y., and Liou, M., "Data Mining for Evolutionary Design Optimization," AIAA Paper 2004-2143, Portland, OR, June 28-July 1,2004.
  13. Lian, Y., Liou, M., and Oyama, A., "An Enhanced Evolutionary Algorithm with a Surrogate Model," Proceeding of Genetic and Evolutionary Computation Conference, Seattle, WA, June 2004.
  14. Zhang, B.N., Lian, Y., and Shyy, W., "Proper Orthogonal  Decomposition for Three-Dimensional Membrane Wing Aerodynamics," AIAA Paper 2003-3917, Orlando, FL, June 2003.
  15. Viieru, D., Lian, Y., and Shyy, W., "Investigation of Tip Vortex on Aerodynamic Performance of a Micro Air Vehicle," AIAA Paper 2003-3597, Orlando, FL, June 2003.
  16. Lian, Y. and Shyy, W., "Three-Dimensional Fluid-Structure Interactions of a Membrane Wing for Micro Air Vehicle Applications," AIAA Paper 2003-1726, Norfolk, VA, April 2003.
  17. Lian, Y., Shyy, W. and Haftka, R., "Shape Optimization of a Membrane Wing for Micro Air Vehicles," AIAA Paper 2003-0106, Reno, NV, January 2003.
  18.  Lian, Y., Shyy, W., Ifju, P. and Verron, E.,"A Computational Model for Coupled Membrane-Fluid Dynamics," AIAA Paper 2002-2972, St. Louis, MO, June 2002.
  19. Kamakoti, R., Lian, Y., Regisford, S., Kurdila, A. and Shyy, W., "Computational Aeroelasticity using a Pressure-based Solver," AIAA Paper 2002-0869, Reno, NV, January 2002.
  20. Ifju, P., Jenkins, D., Ettinger, S., Lian, Y. and Shyy, W., "Flexible-Wing-Based Micro Air Vehicles," AIAA Paper 2002-0705, Reno, NV, January 2002.
  21. Lian, Y., Steen, J., Trygg-Wilander, M., and Shyy, W., "Low Reynolds Number Turbulent Flows around a Dynamically Shaped Airfoil," AIAA Paper 2001-2723, Anaheim, CA, June 2001.
  22. Fuentes, C., He, X., Carroll, B., Lian, Y. and Shyy, W., "Low Reynolds Number Flows Around an Airfoil with a Movable Flap, Part 1: Experiments," AIAA Paper 2000-2239, Denver, CO, June 2000.
  23. He, X., Fuentes, C., Shyy, W., Lian, Y. and Carroll, B., "Computation of Transitional Flows around an Airfoil with a Movable Flap," AIAA Paper 2000-2240, Denver, CO, June 2000.
Document Actions
Personal tools