Professor Rho Shin Myong
Tel:+82-55-772-1645/Fax: +82-55-772-1580/Office GNU Building 403 Room 205
E-mail: myong@gnu.ac.kr
▶ Education
Ph. D.: Aerospace Engineering, University of Michigan at Ann Arbor (1996. 8; Advisor P. L. Roe)
MS: Aeronautical Engineering, Seoul National University (1989. 2)
BS: Aeronautical Engineering, Seoul National University(1987. 2)
▶ Experiences
1999. 3 - Present: Professor (Assistant, Associate, Full), Gyeongsang National University
2004. 7 - 2005. 2: Visiting Professor, University of Chicago
2004. 1 - 2004. 6: Visiting Scholar, University of Strathclyde (UK)
2000. 1 - 2000. 2: Visiting Scholar, IMA (Institute for Mathematics Applications), University of Minnesota
1997. 2 - 1999. 2: Research Associate, NASA Goddard Space Flight Center
1990. 3 - 1991. 8: Researcher, KIST (Korea)
▶ Principal Areas of Research Interests
Aerodynamc Analysis and Design (Applied Aerodynamics)
Computational Fluid Dynamics (CFD)
Non-equilibrium Fluid Dynamics (Micro/Nano Scale Gases and Hypersonics)
Aircraft/Wind-Turbine Icing and Certification, Survivability and RF/IR Stealth Technology
▶ Journal Editorial and Scientific Committee Services
Associate editor, Communications in Computational Physics (Global Science Press)
Editorial board member, International Journal of Computational Fluid Dynamics
International scientific committee member, 2nd & 3rd Micro and Nano Flows Conference
▶ Conference and Invited Colloquium Talk
Keynote Lecture, 1st European Conference on Gas Micro Flows, 2012 (June)
Samsung Heavy Industries LTD, 2011 (July)
Atmospheric Ice Accretion on Wind Turbine Blades: Numerical Modeling and Anti/De-Icing System
McGill University, 2011 (March)
Pushing the Limits of Continuum Fluid Mechanics and Going beyond the Navier-Stokes-Fourier
48th AIAA Aerospace Sciences Meeting 2010 (January)
Workshop on Moment Methods in Kinetic Theory 2008 (November)
KAIST Industrial Mathematics Initiative 2006 (July 26-29)
25th International Symposium on Rarefied Gas Dynamics 2006 (July)
Modeling of Gaseous Expansion in Free Jet and Microchannel Flows Using the Modified Moment Method
Korea Aerospace Industries LTD 2006 (June)
Computational Electromagnetics (CEM) for Radar Signature Reduction of Aircraft (38 pages)
Korea Aerospace Industries LTD 2006 (May)
An Introduction to RF and IR Stealth Technology (17/43 pages)
University of Chicago (Modeling Micro Flows: Surface Chemistry, Boltzmann Equation, and Irreversible Thermodynamics, Computations in Science Seminars, Jan. 2005)
University of Strathclyde
European Applied Mathematics
IMA, University of Minnesota
▶ Scientific Contributions and C. V.
▷ C. V.
▶ Principal Publications
▷ Thesis & Book
Ph.D. Thesis:. Theoretical and Computational Investigations of Nonlinear Waves in Magnetohydro
dynamics, 1996
▷ International Journal Papers
Le, N. T. P., White, C., Reese, J. M., Myong, R. S., Langmuir-Maxwell and Langmuir-Smoluchowski Boundary Conditions for Thermal Gas Flow Simulations in Hypersonic Aerodynamics, International Journal of Heat and Mass Transfer, Vol. 55, Nos. 19-20, pp. 4929-5378, 2012. 09.
Mohammadzadeh, A., Roohi, E., Niazmand, H., Stefanov, S., Myong, R. S., Thermal and Second-Law Analysis of a Micro- or Nanocavity Using Direct-Simulation Monte Carlo, Physical Review E, Vol. 85, No. 5, 056310, 2012. 05.
Yang, Y. R., Jung, S. K., Cho, T. H., Myong, R. S. Aerodynamic Shape Optimization of a Canard-Controlled Missile Using Trajectory-Dependent Aerodynamic Coefficients, Journal of Spacecraft and Rockets, Vol. 49, No. 2, pp. 243-249, 2012. 03-04.
Myong, R. S., Impact of Computational Physics on Multi-scale CFD and Related Numerical Algorithms, Computers & Fluids, Vol. 45, No. 1, pp. 64-69, 2011. 06.
Jung, S. K., Shin, S., Myong, R. S., Cho, T. H., An Efficient CFD-Based Method for Aircraft Icing Simulation Using a Reduced Order Model, Journal of Mechanical Science and Technology, Vol. 25, No. 3, pp. 703-711, 2011. 03.
Myong, R. S., A Full Analytical Solution for the Force-Driven Compressible Poiseuille Gas Flow Based on a Nonlinear Coupled Constitutive Relation, Physics of Fluids, Vol. 23, No. 1, 012002, 2011. 01.
Hu, Z. M., Myong, R. S., Yang, Y. R., Cho, T. H., Reconsideration of Inviscid Shock Interactions and Transition Phenomena on Double-Wedge Geometries in a M∞ = 9 Hypersonic Flow, Theoretical and Computational Fluid Dynamics, Vol. 24, No. 6, pp. 551-564, 2010. 12.
Hu, Z. M., Gao, Y.L., Myong, R. S., Dou, H. S., and Khoo, B. C., Geometric criterion for RR↔MR transition in hypersonic double-wedge flows, Physics of Fluids, Vol. 22, No.1, 016101, 2010. 01.
Myong, R. S., Coupled nonlinear constitutive models for rarefied and microscale gas flows : Subtle interplay of kinematics and dissipation effects, Continuum Mechanics and Thermodynamics, Vol. 21, No. 5, pp. 389-399, 2009. 11.
Hu, Z. M., Myong, R. S., Kim, M. S., Cho, T. H., Downstream Flow Condition Effects on the RR → MR Transition of asymmetrc Shock Waves in Steady Flows, Journal of Fluid Mechanics, Vol. 620, pp. 43-62, 2009. 2.
Hu, Z. M., Wang, C., Zhang, Y., Myong, R. S., Computational Confirmation of an Abnormal Mach Reflection Wave Configuration, Physics of Fluids, Vol. 21, 011702, 2009. 1.
Hu, Z., Kim, M. S., Myong, R. S., Cho, T. H., ON the RR → MR transition of Asymmetric Shock Waves in Steady Flows, Shock Waves, Vol. 18, No. 5, pp. 419-423, 2008. 10.
Hu, Z., Myong, R. S., Wang, C., Cho, T. H., Liang, Z. L., Numerical Study of the Oscillations Induced by Shock/Shock Interaction in Hypersonic Double-Wedge Flows, Shock Waves, Vol. 18, No. 1, pp. 41-51, 2008. 6.
Hu, Z., Jiang, Z., Myong, R. S., Cho, T., Numerical Analysis of Spatial Evolution of the Small Signal Gain in a Chemical Oxygen-Iodine Laser Operating without Primary Buffer Gas, Optics and Laser Technology, Vol. 40, pp. 13-20, 2008. 2.
Myong, R. S., Lockerby, D. A., and Reese, J. M., The Effect of Gaseous Slip on Microscale Heat Transfer: An Extended Graetz Problem, International Journal of Heat and Mass Transfer, Vol. 49, No. 15-16 (July), pp. 2502-2513, 2006.
Myong, R. S., Reese, J. M., Barber, R. W., and Emerson, D. R., Velocity Slip in Microscale Cylindrical Couette Flow: The Langmuir Model, Physics of Fluids, Vol. 17, 087105, 2005.
Myong, R. S., Gaseous Slip Model Based on the Langmuir Adsorption Isotherm, Physics of Fluids, Vol. 16, No. 1, pp. 104-117, 2004.
Myong, R. S., A Generalized Hydrodynamic Computational Model for Rarefied and Microscale Diatomic Gas Flows, J. of Computational Physics, Vol. 195, No. 2, pp. 655-676, 2004.
Myong, R. S., A Computational Method for Eu's Generalized Hydrodynamic Equations of Rarefied and Microscale Gasdynamics, Journal of Computational Physics, Vol. 168, pp. 47-72, 2001.
Myong, R. S., Thermodynamically Consistent Hydrodynamic Computational Models for High-Knudsen-Number gas flows, Physics of Fluids, Vol. 11, No. 9, pp. 2788-2802, 1999.
Myong, R. S. and Roe, P. L., On Godunov-Type Schemes for Magnetohydrodynamics. Part 1. A Model System, Journal of Computational Physics, Vol. 147, pp. 545-567, 1998.
Myong, R. S., Analytical Results on MHD Intermediate Shocks, Geophysical Research Letters, Vol. 24, No. 22, pp. 2929-2932, 1997.
Myong, R. S. and Roe, P. L., Shock Waves and Rarefaction Waves in Magnetohydrodynamics: I. A Model System, Journal of Plasma Physics, Vol. 58, pp. 485-519, 1997.
Myong, R. S. and Roe, P. L., Shock Waves and Rarefaction Waves in Magnetohydrodynamics: II. The MHD System, Journal of Plasma Physics, Vol. 58, pp. 521-552, 1997.
▷ Domestic Journal Papers
K. Y. Jung et al., Computational Prediction of Ice Accretion around a Rotorcraft Air Intake, J. of Computational Fluids Engineering, Vol. 17, No. 2, pp. 100-106, 2012. 06.
Young-Gab An et al.. Scaling Methods for Icing Wind Tunnel Test, J. of The Korean Society for Aeronautical and Space Sciences, Vol. 40, No. 2, pp. 146-156, 2012. 2.
Y. J. Kang et al., Computational Design of a Fluted Nozzle for Achieving Target Aerodynamic Performance, Journal of Computational Fluids Engineering, Vol. 16, No. 3, pp. 1-7, 2011. 9.
S. H. Chun et al., Computational Investigation of Nozzle Flowfields at Various Flight Conditions for Aircraft Infrared Signature Analysis, Journal of Computational Fluids Engineering, Vol. 16, No. 3, pp. 15-21, 2011. 9.
Moon, H. et al., Computation of Flowfield and Infrared Signature in Aircraft Exhaust System for IR Reduction Design, J. of The Korean Society for Aeronautical and Space Sciences, Vol. 39, No. 7, pp. 652-659, 2011. 7.
Jung, S. K. et al., A Study on Truncated Flapped Airfoil for Efficient Icing Wind Tunnel Test, J. of The Korean Society for Aeronautical and Space Sciences, Vol. 39, No. 6, pp. 481-486, 2011. 6.
Yang, Y. R. et al., Range Sensitivity Analysis of a Canard Controlled Missile, Journal of the Korea Institute of Military Science and Technology, Vol. 14, No. 1, pp. 39-48, 2011.2
Yang, Y. R. et al., A Prediction Study on the Roll Lock-in Phenomena of Freely Spinning Tailfins, J. of The Korean Society for Aeronautical and Space Sciences, Vol. 38, No. 9, pp. 849-855, 2010. 9.
Jung, S. K. et al., An Eulerian-Based Droplet Impingement and Ice Accretion Code for Aircraft Icing Prediction, Journal of Computational Fluids Engineering, Vol. 15, No. 2, pp. 71-78, 2010. 6.
Jung, S. K. et al., An Investigation of Icing Effects on the Aerodynamic Characteristics of KC-100 Aircraft, J. of The Korean Society for Aeronautical and Space Sciences, Vol. 38, No. 6, pp. 530-536, 2010. 6.
Yang, Y. R. et al., A Numerical Study on the Roll Lock-In of a Canard-Controlled Missile with Freely Spinning Tailfins, Journal of Computational Fluids Engineering, Vol. 14, No. 4, pp. 48-55, 2009. 12.
Jung, S. K. et al., Efficient Analysis of the Aerodynamic Characteristics of Rotor Blade Using Reduced Order Model Based on Proper Orthogonal Decomposition Method, J. of The Korean Society for Aeronautical and Space Sciences, Vol. 37, No. 11, pp. 1073-1079, 2009. 11.
Yang, Y. R. et al., The Reynolds Number Effects on the Projectile with an Altitude Change, J. of The Korean Society for Aeronautical and Space Sciences, Vol. 12, No. 5, pp. 683-688, 2009. 10.
Hoang, A. D. et al., Implementation of Velocity Slip Models in a Finite Element Numerical Code for Microscale Fluid Simulations, Journal of Computational Fluids Engineering, Vol. 14, No. 2, pp. 46-51, 2009. 6.
Yang, Y. R. et al., An External Shape Optimization Study to Maximize the Range of a Guided Missile in Atmospheric Flight, J. of The Korean Society for Aeronautical and Space Sciences, Vol. 37, No. 6, pp. 519-526, 2009. 6.
Jung, S. K. et al., An Efficient Global Optimization Method for Reducing the Wave Drag in Transonic Regime, J. of The Korean Society for Aeronautical and Space Sciences, Vol. 37, No. 3, pp. 248-254, 2009. 3.
Jung, S. K. et al., A Static Fluid-Structure Interaction Analysis System Based on the Navier-Stokes Equations for the prediction of Aerodynamic Characteristics of Aircraft, J. of The Korean Society for Aeronautical and Space Sciences, Vol. 36, No. 6, pp. 532-540, 2008. 6.
Kim, D. J. et al. Design of Pitot-Tube Configuration Using CFD Analysis and Optimization Techniques, Transactions of The Korean Society of Mechanical Engineers - B, Vol. 32, No. 5, pp. 392-399, 2008. 5.
Yang, Y. R. et al., Aerodynamic Characteristics of a Canard-Controlled Missile with Freely Spinning Tailfins Using A Semi-Empirical Method and a CFD Code, J. of The Korean Society for Aeronautical and Space Sciences, Vol. 36, No. 3, pp. 220-228, 2008. 3.
Park, M. J. et al., An Integrated System for Aerodynamic, Structural, and RF Stealth Analysis of Flying Vehicles, J. of The Korean Society for Aeronautical and Space Sciences, Vol. 36, No. 1, pp. 86-91, 2008. 1.
Seo, J. H. et al. A Computational Study on the Characteristics of Flowfields in Micronozzles, Journal of Computational Fluids Engineering (Korean Society of Computational Fluids Engineering), Vol. 12, No. 4, pp. 38-43, 2007. 12.
Hoang, A. D. et al., Development of a Three-Dimensional Multi-Block Structured Grid Deformation Code for Complex Configuration, Journal of Computational Fluids Engineering (Korean Society of Computational Fluids Engineering), Vol. 12, No. 4, pp. 28-37, 2007. 12.
Jung, S. C., Kim, Y.H., Oh, H. Y., Huh,H. I., Myong, R. S., Performance Evaluation of Micro-nozzle Using Cold Gas Propulsion System, Journal of the Korean Society of Propulsion Engineers, Vol.11, No.6, pp.42-49, 2007.12.
Hu, Z. M. et al., A Robust Scheme for the Multicomponent Reactive Gas Flows in the Presence of Shock Waves, Journal of Computational Fluids Engineering (Korean Society of Computational Fluids Engineering), Vol. 12, No. 1, pp. 60-67, 2007. 3.
Myong, R. S. and Cho, T. H., Development of a Computational Electromagnetics Code for Radar Cross Section Calculations of Flying Vehicles, J. of Korean Society for Aeronautical and Space Sciences, Vol. 33, No. 4, pp. 1-6, 2005.
Han, M. S. et al., Analysis of the Aerodynamic Characteristics of Missile Configurations Using a Semi-Empirical Method, J. of Korean Society for Aeronautical and Space Sciences, Vol. 33, No. 3, pp. 26-31, 2005.
Pack, K. C. and Myong, R. S., Investigation of Ice Impacts on Aluminum Skin Structure, J. of Korean Society for Aeronautical and Space Sciences, Vol. 31, No. 5, pp. 110-115, 2003.
Myong, R. S. and Cho, S. Y., Development of Wall Slip Models for Rarefied Gas and MEMS Thermal Fluid Flows, J. of Korean Society for Aeronautical and Space Sciences, Vol. 30, No. 7, pp. 90-97, 2002.
Myong, R. S., Numerical Analysis of Rarefied Hypersonic Flows Using Generalized Hydrodynamic Models for Diatomic Gases, J. of Korean Society for Aeronautical and Space Sciences, Vol. 30, No. 5, pp. 32-40, 2002.
Myong, R. S., Analysis of Rarefied and MEMS Gas Flows Using Thermodynamically Consistent Nonequilibrium Hydrodynamic Models, J. of Korean Society for Aeronautical and Space Sciences, Vol. 28, No. 4, pp. 35-47, 2000.