Proceedings of the 34th International Symposium on Shock Waves, Volume 1: Fundamentals (eBook, PDF)

ISSW34, July 16-21 2023, Daegu, South Korea
Redaktion: Myong, Rho Shin; Kim, Heuy Dong

• Format: PDF

Produktbeschreibung

Shock waves are strong pressure waves resulting from irreversible processes in elastic media, including gases, liquids, or solids, generated by supersonic aircraft, explosions, or phenomena that cause rapid changes in pressure. The conference proceedings of the 34th International Symposium on Shock Waves (ISSW34), held in Daegu, Korea, in 2023, cover theoretical, experimental, and computational studies of these shock waves and associated phenomena, addressing both fundamental and applied aspects. They serve as the most up-to-date resource for physicists, chemists, engineers, and applied mathematicians involved in shock wave research.

The three-volume set present the latest studies on diverse topics, including shock waves in gases, liquids, and solids, as well as in internal flows, detonation, supersonic and hypersonic flows, nozzle flows, and supersonic jet. It also explores emerging topics such as advanced shock tube design and application, recent development in diagnostics and flow visualization, shock waves in multiphase flows, and detonation engines.

Volume 1 contains 52 articles covering the fundamentals of shock waves, including physical and chemical properties of shock waves, shock-vortex interaction, and numerical and experimental techniques.

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Produktdetails

• Verlag: Springer Nature Singapore
• Seitenzahl: 601
• Erscheinungstermin: 18. Oktober 2025
• Englisch
• ISBN-13: 9789819647675
• Artikelnr.: 75703216

Autorenporträt

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.

Inhaltsangabe

Shock Wave Boundary Layer Interactions Over a Forward Facing Step at Mach 6.- Effects of Reynolds Number and Ramp Angle on Gortler Vortices over a Compression Ramp.- Large Eddy Simulation of the Control of the Inlet Buzz Phenomenon in a Supersonic Air Inlet.- On The Nature Of The Fishtail Shock Shock Interaction In The Transonic Flow Past A NACA0012 Profile.- Shock fitted Calculation Of Steady Mach Reflections In Overexpanded Nozzles Using Structured Grids.- Frequency Analysis of Heat-Transfer signals in Hypersonic Transitional and Turbulent Boundary Layers.- Fifth Order Bound-, Positivity, and Equilibrium Preserving Affine Invariant AWENO Scheme for Two Medium based Model of Stiffened Gas.- Investigation of shock-shock interaction in variable Mach number flow.- Dynamic Interactions Between an Oblique Shock and a Moving Cylinder.- Shock Tube Chemiluminescence and Spectroscopic CO Measurements of Norbornadiene.- Assessment of Axial Variations of Temperature and Enthalpy in a NASA Arc Jet using Laser Absorption of Atomic Oxygen and Nitrogen.- Global Instability of the Interaction Between an Oblique Shock and a Laminar Boundary Layer.- Analysis of High Enthalpy Shock Boundary Layer Interaction using a Shock Strength Dependent Turbulence Model.- Measurements of Disturbances Generated Over Hypersonic Boundary Layers with Shock Interactions.- Numerical Simulation of Supersonic Dusty Gas Flow
Over a Cylinder in the Eulerian Lagrangian Framework.- Stability of Planar, Cylindrical and Spherical Steady Shocks.- Richtmyer Meshkov Instability Coupled with a Chemical Reaction.- Mach Evolution of the Cylinder Wake Flow Bifurcations.- Coexistence of Different Mechanisms in Shock Wave/Turbulent Boundary Layer Interactions.- Navier-Stokes Simulation of a Strong Shock Vortex Interaction.