Shock-Tube Facility Non-Ideality Dependence.- Investigation of Compressible Flow and Wave Phenomena in Hyperloop System.- Experimental Research on the Submillisecond Condensation of Water Vapour Based on Absorption Spectroscopy.- Characteristics of shock wave depending on electrical parameters and gap spacing in underwater double gap discharge.- Influence of Ambient Pressure on Shock Wave Intensity for Vertical Well Cleaning.- Optimization of Split Hopkinson Pressure Bar diagnostics for characterization of granular materials.- Correlation between Circuit Parameters and Peak Pressure of Shock Wave Generated by Underwater Electrical Wire Explosion.- Passive Control of Pseudo-Shock Wave using Bypass Flow Passage.- Restricted Shock Separation in Out of Round TOP Nozzles.- Incident Shock-Wave/Turbulent Boundary Layer Interactions on Concave Elliptical Surfaces.- Generation and behavior of underwater shock waves and microbubbles produced by metal plate discharge.- Flow Separation Control in Over Expanded Supersonic Planar Nozzles.- Experimental Study and Numerical Simulation of a Surface Sliding Discharge in a Supersonic Airflow with a Separation Zone.- Measurement of blast wave-induced strain using FBG sensor inside shock tube.- Towards single cell shock wave mediated drug delivery.- The Use of 3D printed Models in Gas Dynamics Research.- Production of blast waves with the second shock, and experiments on blast diffraction.- Development of Pressure Distribution Measurement Technique on Free Flight Object Surface at Transonic Speed.- Experimental Investigation of a Curved Compression Ramp Air Intake at Mach 6.- Numerical Study of Blockage Effects on Shock Induced Motion of a Solid Body in a Shock Tube.- Shock Induced Resuspension of Poly layered Particles.- ES BGK model with internal energy relaxation: application to hypersonic flow around a cylinder.- Unimolecular decomposition of trans-Hydrindane in a single pulse shock tube.- Near Body Shock Wave Motion for an Accelerating Slender Body.- Dependence of Blast wave Mitigation by Periodic Obstacles in a Straight Tube on Height of Obstacles.- Influence of the impinging shock location along the separated shear layer of a supersonic confined cavity.- A comparative study on the blast wave mitigation in different composite materials using shock tube experiments.- Aluminium Particle Enrichment of Hemispherical Charges.- Computations on Control of Impinging Shock Boundary Layer Interaction using Boundary Layer Bleeding.- Numerical Simulation of Blast Wave Propagation in a Large Urban Environment: the 2020 Beirut Explosion.- On shockwave vortex interaction and configuration in interblade channel with PSC.- Optimal Parameters for the Regular Interaction of a Shock Wave Striking a Rigid Plane Wall.- Effect of conical free stream on shock detachment and heat flux in hypersonic blunt body flows.- Unsteady Numerical Studies on Spinning Cone at Different Flow Regimes.- FSI Analysis of Shock Wave Impinging on a Solid Object.- Focussing of weak conical shocks at nearly glancing incidence.- Mode decomposition of three dimensional oblique shock wave/turbulent boundary layer interactions in a subscale overexpanded planar nozzle.- Flat Plate Flutter in a Supersonic Flow Field.- Acoustic Pulse Generation in Collapse of a Liquid Cavity.- Effect of pressure of shock wave induced by Wire Explosion on Particle Size distribution of Powdered Wire in Air.- Evolution of shock accelerated multi layer gas cylinder with different Mach numbers.- Effect of substrate surface on testing parameters and thermal per-formance of thin film gauges.-
Formation of a Blast Wave during Supersonic Impact of a Reactive Metal Projectile.- A Study on the Effect of Ground Vibration Control of Blasting Method Using Explosive Distributed Charging Technique.- Flow Control on a Supersonic Compression Corner with the Periodic Activations of Nanosecond Surface Dielectric Barrier Discharge Plasma Actuators.- Measurement of the blast environment during military weapons training using BlackBox Biometrics (B3) Blast Gauges and pencil probes.- Depolymerization study on Chitosan Biopolymer subjected to Shock Wave Impact.- Investigation of Aerospike-Induced Flow Instability.- Observation and measurements of femto second laser induced micro shock wave propagation and bubble behavior for development of micro scale regenerative cell culture systems.- Numerical and Experimental Investigation of MHD Shock Layer Enlargement in JAXA HEK X Giant Expansion Tube.- Numerical Study of a Converging Novel Shock Tube for Biomedical Application.- Blast Mitigation in Semi Confined Volume through Fireball Extinction by Water.- Shock Wave Instability Effects in Transonic Flutter Cascade.- Shape Characterisation of Curved Incident Shock Waves in Axisymmetric Ring Intakes with Curvature.- Visualization of Under-Expanded Cryogenic Jet Impinging on a Convex Surface.
Rho Shin Myong is a professor at the school of mechanical and aerospace engineering, Gyeongsang National University in Jinju, South Korea. He is the director of the (Engineering) Research Center for Aircraft Core Technology at Gyeongsang National University. He received his B.S. and M.S. degrees in aeronautical engineering from Seoul National University in 1987 and 1989, respectively. He received his Ph.D. degree in aerospace engineering from the University of Michigan in 1996. Prior to the present position, he worked at the NASA Goddard Space Flight Center from 1997 to 1999 as a National Research Council (NRC) research associate. He is an editorial board member of the International Journal of Computational Fluid Dynamics and serves as a scientific committee member for several international symposiums including Shock Waves.
His major research area includes theoretical and computational studies of shock waves in rarefied gases, magnetohydrodynamics, chemically reacting gases, and dusty and granular gases. Additionally, he conducts research on shock-vortex interaction by developing a mixed modal discontinuous Galerkin method. Recently, he has developed a pure quantum algorithm for nonlinear partial differential equations to govern high-speed compressible gas flows including self-steepening shock waves.
Heuy Dong Kim is a professor at the Department of Mechanical Engineering, the College of Engineering, Andong National University in South Korea. He received his Ph.D. in engineering from Kyushu University in Fukuoka, Japan in 1991. Before joining Andong National University in 1993, he was a lecturer at Kyushu University. He has published over 390 papers in international journals and has actively contributed to the academic community by organizing 13 international conferences. Notably, he played a key role in organizing the 34th International Symposium on Shock Waves (ISSW34) in Daegu, South Korea, in July 2023 and the International Congress of Theoretical and Applied Mechanics (ICTAM 2024) in August 2024. In recognition of his contributions, he has received over 15 academic and achievement awards from South Korean government institutions.
His major research area includes the interaction between shock waves and boundary layer flows, unsteady compressible flows, supersonic jets, high-speed fluid machinery, and wave phenomena in high-speed railway tunnels. He primarily investigates compressible internal flows through experimental and numerical analysis. Additionally, he conducts research on shock wave dynamics and high-speed aerodynamics using shock tubes, two-stage light gas guns, and ballistic ranges. In recent years, he has shown a growing interest in complex compressible flows, such as gas-liquid and gas-solid particles, phase-change phenomena, as well as electrofuels, also known as e-fuels. He is also jointly working on medical shock wave therapy.
