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Proceedings of the 34th International Symposium on Shock Waves.ISSW34, July 16-21 2023, Daegu, South Korea /Volume 2,Applications 1

Record Type:	Electronic resources : Monograph/item
Title/Author:	Proceedings of the 34th International Symposium on Shock Waves.edited by Rho Shin Myong, Heuy Dong Kim.
Reminder of title:	ISSW34, July 16-21 2023, Daegu, South Korea /
remainder title:	Applications 1
other author:	Myong, Rho Shin.
corporate name:
Published:	Singapore :Springer Nature Singapore :2025.
Description:	xii, 617 p. :ill., digital ;24 cm.
Contained By:	Springer Nature eBook
Subject:	Shock wavesCongresses.
Online resource:	https://doi.org/10.1007/978-981-96-4771-2
ISBN:	9789819647712$q(electronic bk.)

Proceedings of the 34th International Symposium on Shock Waves.ISSW34, July 16-21 2023, Daegu, South Korea /Volume 2,Applications 1
Proceedings of the 34th International Symposium on Shock Waves.ISSW34, July 16-21 2023, Daegu, South Korea /Volume 2,Applications 1[electronic resource] :Applications 1edited by Rho Shin Myong, Heuy Dong Kim. - Singapore :Springer Nature Singapore :2025. - xii, 617 p. :ill., digital ;24 cm.

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.

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.

ISBN: 9789819647712$q(electronic bk.)

Standard No.: 10.1007/978-981-96-4771-2doiSubjects--Topical Terms:

404861
Shock waves
--Congresses.

LC Class. No.: QC168.85.S45 / I58 2023

Dewey Class. No.: 531.1133

Proceedings of the 34th International Symposium on Shock Waves.ISSW34, July 16-21 2023, Daegu, South Korea /Volume 2,Applications 1
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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.
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