| 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: |
International Symposium on Shock Waves |
| Published: |
Singapore :Springer Nature Singapore : : 2025., |
| Description: |
xii, 617 p. :ill., digital ;24 cm. |
| [NT 15003449]: |
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. |
| Contained By: |
Springer Nature eBook |
| Subject: |
Shock waves - Congresses. - |
| Online resource: |
https://doi.org/10.1007/978-981-96-4771-2 |
| ISBN: |
9789819647712 |