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

Name: Proceedings of the 34th International Symposium on Shock Waves, Volume 2: Applications 1
Brand: Springer
Availability: OutOfStock
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By Myong, Rho Shin

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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 Curvatur

Product details

Number of Pages:: 632
Release Date:: 2025-10-02
Publication Date:: 2025-10-02
Publisher:: Springer
Languages:: Original: English
ISBN10:: 9819647703
ISBN13:: 9789819647705
GPSR Manufacturer Reference:: [email protected]
Weight:: 1101 g
Height:: 16 cm
Width:: 24.1 cm
Thickness:: 4 cm

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