Professor Rho Shin Myong

                                          

 

 

 

▶ 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

▶ Conference and Invited Colloquium Talk

 

▶ Scientific Contributions and C. V.

 

        Scientific Contributions

 

        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., Xiao, H., Myong, R. S., A Triangular Discontinuous Galerkin Method for Non-Newtonian Implicit Constitutive Models of Rarefied and Microscale Gases, Journal of Computational Physics, Vol. 273, pp. 160-184, 2014. 09.

 

Myong, R. S., On the high Mach number shock structure singularity caused by overreach of Maxwellian molecules, Physics of Fluids, Vol. 26, No. 5, 056102, 2014. 05 (Full Paper).

 

Myong, R. S., Analytical Solutions of the Shock Structure Thickness and Asymmetry in the Navier-Stokes-Fourier Framework, Vol. 52, No. 5, pp. 1075-1080, 2014. 05.

 

Balaj, M., Roohi, E., Akhlaghi, H., Myong, R. S., Investigation of Convective Heat Transfer through Constant Wall Heat Flux Micro/Nano Channels using DSMC, International Journal of Heat and Mass Transfer, Vol. 71, pp. 633-638, 2014. 04.

 

Ranjith,R., Myong, R. S., Lee, S., Computational Investigation of Lightning Strike Effects on Aircraft Components, International Journal of Aeronautical and Space Science, Vol. 15, No. 1, pp. 44-53, 2014. 01.

 

Jung, S. K., Myong, R. S., A Second-Order Positivity-Preserving Finite Volume Upwind Scheme for Air-Mixed Droplet Flow in Atmospheric Icing, Computers & Fluids, Vol. 86, pp. 459-469, 2013. 11.

 

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

 

 

J. H. Park et al., Aerodynamic Characteristics of Wind Turbine Blades and Performance Changes due to Atmospheric Icing, J. of The Korean Society for Aeronautical and Space Sciences, Vol. 42, No. 2, pp. 134-143, 2014. 02.

 

D. W. Kang et al., Investigation of Aircraft Plume IR Signature for Various Nozzle Configurations and Atmospheric Conditions , J. of The Korean Society for Aeronautical and Space Sciences, Vol. 42, No. 1, pp. 10-19, 2014. 01.

 

D. W. Kang et al., Computational Investigation of the Effect of UAV Engine Nozzle Configuration on Infrared Signature, J. of The Korean Society for Aeronautical and Space Sciences, Vol. 41, No. 10, pp. 779-787, 2013.10.

 

J. H. Park et al., Computational Prediction of Icing Effects on Aerodynamic Characteristics of a Wind Turbine Blade, J. of Computational Fluids Engineering, Vol. 18, No. 3, pp. 51-59, 2013. 09.

 

K. Y. Jung et al., A Three-Dimensional Unstructured Finite Volume Method for Analysis of Droplet Impingement in Icing, J. of Computational Fluids Engineering, Vol. 18, No. 2, pp. 41-49, 2013. 06.

 

G. B. Ahn et al., Investigation of the Performance of Anti-Icing System of a Rotorcraft Engine Air Intake, J. of The Korean Society for Aeronautical and Space Sciences, Vol. 41, No. 4, pp. 253-260, 2013. 04.

 

J. Y. Kim et al., Computational Investigation of the Effect of Various Flight Conditions on Plume Infrared Signature, J. of The Korean Society for Aeronautical and Space Sciences, Vol. 41, No. 3, pp. 185-193, 2013. 03.

 

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.