Proceedings of the 34th International Symposium on Shock Waves, Volume 2: Applications 1

ISSW34, July 16-21 2023, Daegu, South Korea
Erscheinungsjahr 2025
ISBN: 978-981-964770-5
Verlag: Springer

Buch, Englisch, 617 Seiten, Format (B × H): 160 mm x 241 mm, Gewicht: 1101 g

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 2 contains 57 articles covering the applications (part 1) of shock waves to various fields encompassing mechanical engineering, aerospace engineering, space sciences, geosciences, materials sciences, life sciences, and medicine.

Zielgruppe

Research

Autoren/Hrsg.

Myong, Rho Shin

Kim, Heuy Dong

Fachgebiete

• Naturwissenschaften Physik Mechanik
• Technische Wissenschaften Maschinenbau | Werkstoffkunde Technische Mechanik | Werkstoffkunde Strömungslehre
• Technische Wissenschaften Sonstige Technologien | Angewandte Technik Akustik, Tontechnik
• Technische Wissenschaften Sonstige Technologien | Angewandte Technik Astronautik
• Naturwissenschaften Chemie Physikalische Chemie
• Technische Wissenschaften Verkehrstechnik | Transportgewerbe Luft- und Raumfahrttechnik, Luftverkehr

Inhaltsverzeichnis

Finite Element Simulation of the Second Sound Wave in a Chamber Annulus Wall of a Rotating Detonation Engine.- Detonation Flame Arrestor Design and Performance Evaluation Using Experimental and Numerical Methods.- Streamline-Traced Inlet Design and Integration with Rotating Detonation Engines.- Numerical Investigation of a Scramjet Engine with Two Opposing Cavities.- Numerical Analysis of Scramjet Inlet and Isolator According to the Heat Transfer Boundary Condition.- Multi Wave Mode Analysis of Methane Oxygen Rotating Detonation.- Characteristics of Supercritical JetA injection in Supersonic Crossflow.- Wave Dynamics in a Small Scale Continuous Detonation Combustor.- Shuttling Transverse Detonation Waves in a Linear Channel.-  Hinge Line Suction for the Investigation of Streamwise Vortices in a Hypersonic Compression Corner Flow.- Unsteadiness of the Cavity Shear Layer at a Hypersonic Speed.- Magnetohydrodynamic experiments conducted in a detonation driven high enthalpy shock tunnel.- Experimental and Numerical Investigation on the Longitudinal Stage Separation for Parallel staged Two stage to orbit Vehicle.- Using supersonic flows for separating carbon dioxide from industrial gaseous effluents.- Effect of Magnetohydrodynamic Aerobraking on Flow Field Surrounding an Earth Re Entry Capsule.- Unstart Prediction of Scramjet Engine for Variable Mach Number.- Shock Tube Study of HTPB Ignition Using an Endwall Injector.- Initial evolution of drop post weak shockwave interaction in the bag regime.- Unsteady Heating Experiments of Silicon-based Heat resistant Materials in High enthalpy Flows Simulating Earth's Atmospheric Reentry Environments.- Experimental Investigation of RP 1 Ignition Delay Time at Low Pressure Conditions.- Experimental Study on Shock Wave Attenuation Phenomena by Multi layered Wire Gauze Interaction.- Design and Evaluation of Experimental Methods to Study Thermochemical Nonequilibrium in Expanding Flows using TDLAS.- Three Dimensional Computational Study over a Hyper Ballistic Missile body at different Hypersonic Mach Numbers.- Effects of Nozzle Pressure Ratio on Mixing Characteristics of Underexpanded Sonic Twin Jets.- Numerical modeling of blast wave interaction with spatially disseminated burnable liquid simulant.- Vacuum Ultraviolet and Visible Spectral Measurements for Simulated Saturn Entry in the X2 Expansion Tube.- A Numerical Study of Propagation of Rotating Detonation Wave under Non Uniform Inflow Conditions.- Strategies for Supersonic Flow Control Using ns DBD Plasma Actuators.- Numerical Studies of Shuttling Transverse Combustion with Discrete Injection of Premixed Reactant Mixture.- Experimental Investigations on Shock Train Oscillations in an Isolator.- Decay of Shock Waves in Detonation Driven Shock Tubes.- Characterizing the Freestream of the Caltech Hypervelocity Expansion Tube Part I: Facility Gas Dynamics and Simulations.- Characterizing the Freestream of the Caltech Hypervelocity Expansion Tube Part II: Diode Laser Measurements Targeting Atomic Potassium.- Preliminary results for CO 2 recombination for low velocity, high density Mars aerocapture conditions.- A Converging Shock Tube for Strong Shock Interface Interaction Investigation.- Self Excited Oscillation of Normal Shock Wave/Boundary Layer Interaction in Internal Flow.- Shock Train Dynamics in Nozzle Isolator Co-flow Configuration.- Comparison of Static Pressure Measurement Techniques in the T5 Free Piston Reflected Shock Tunnel.- Large Eddy Simulation of Transverse Injection of Hydrogen in A High Enthalpy Crossflow.- Free-piston Driver Performance at High Compression Ratios in the X2 Expansion Tube.-
Curved Body Integrated Diverterless Supersonic Intake (DSI) Design.- A Hybrid High Speed Schlieren and Laser Absorption Diagnostic for Underexpanded Supersonic Jets under Rapid Backpressure Variation.- Interferometric visualization of detonation waves propagating premixed fuel and oxidant jet train.- Effect of Tip Curvature on the Aerodynamic Performance of an Osculating Cone Waverider.- Effect of Premixed Jet Height on Propagation of Detonation Wave inside Linear Detonation Channel.- Analysis on Pressure Gain of Rotating Detonation Engine.- Experimental investigation of Magnetohydrodynamic Aerobraking for High Velocity Mars Entry.- Scaling of Upstream Influence Line Induced by Swept Shock Wave/Turbulent Boundary Layer Interactions on a Concave Half Cylinder.- Backshell Radiative Heating and Shock Layer Kinetic Measurement in NASA’s Electric Arc Shock Tube Facility.- Numerical study on large amplitude oscillatory unstart in a 2D scramjet intake.- Comparison of experimental and numerical results of a methane oxygen rotating detonation engine.- Shock dynamics of sub critical detonation diffraction.- Optical Measurement Technique for Thermo acoustic Pressure Detection in a Combustion Chamber.- Modelling and experiments of the triple point reflection in detonations.- Rapid Scanning Tunable Laser Absorption Measurements of Shock Heated Nonequilibrium Air Species in the NASA Electric Arc Shock Tube.- Experimental Study of Tandem Cavity Scramjet Combustor Ignition using a micro Pulse Detonation Engine.- Detonation attenuation and quenching in hydrogen mixtures after the interaction with cylinders.

Über Autor(innen)

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.