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29th International Symposium on Shock Waves 1 [2015]

1
Hysteresis Phenomena in Reflection of Shock Waves
2
Ten Years of Shock Tube Research at Marseille
3
Driving Forward Innovation in High Speed Aerodynamics and Flow Diagnostics
4
High-Speed Visualization of Compressible Flows – Potential and Limitations
5
Vortex Generation by Shock-Bubble Interaction in Galaxy Clusters
6
Vorticity and Vortex Models in Shock Accelerated Gas Inhomogeneities
7
Successful Development of the Long-Test-Duration Hypervelocity Detonation-Driven Shock Tunnel
8
Shock Waves in Relaxing Condensed Media
9
Evolution of Research – A Case Study
10
Laser-Induced Blast Waves in Air and Their Effect on Monodisperse Droplet Chains of Ethanol and Kerosene
11
Shock Tube Simulation of Low Mach Number Blast Waves
12
Development of a Liquid Blast Tube Facility for Material Testing
13
Analytical Solutions for the Point Source Spherical Blast Wave Propagation with <italic>γ</italic> = 7
14
Explosively-Driven Blast Waves in Small-Diameter Tubes
15
Study on Excessive Pressure of Underwater Shock Wave Generated in Confined Space
16
Time Evolution of the Density Field of a Micro–Explosion Using Background Oriented Schlieren
17
Energy Analysis of a Small-Scale Combustion Driven Blast Tube
18
Shock Interaction Studies on Glass Fibre Reinforced Epoxy Matrix Composites
19
High Energy Concentration by Spherical Converging Shocks in a Shock Tube with Conically Shaped Test Section
20
A Pulsed Detonation Microthruster for Space Applications
21
Constrained Reaction Volume: A New Approach to Studying Reactive Systems in Shock Tubes
22
Laser Absorption Diagnostics for Aldehydes in Shock Tube Kinetics Studies
23
Electronic Excitation Modeling in Chemically Reacting Hypersonic Flows
24
Thermochemical Non-equilibrium Effects on Type VI-V Transition in Hypersonic Double-Wedge Flow
25
A Computationally Efficient Approach to Hypersonic Reacting Flows
26
Thermal Decomposition Study of 3-Carene
27
Experimental Investigation of Propargyl Alcohol Pyrolysis
28
Shock Tube Studies on Thermal Decomposition of 2-Chloroethylbenzene
29
Sensitivity of Shock-Tube Chemiluminescence Measurements to the Optical Setup
30
Thermochemical Nonequilibrium Analysis of Oxygen in Shock Tube Flows
31
Detailed Simulations of Weak-to-Strong Ignition of a H<sub>2</sub>/O<sub>2</sub>/Ar Mixture in Shock-Tubes
32
Experimental Study of Intense Radiation around Si-Based Heat-Resistant Materials in Air Plasma Freejets
33
Laser Absorption Measurements of CO at Elevated Pressures behind Reflected Shock Waves
34
Numerical Study on the Heat Release Distributions of a Supersonic Combustor with Three-Dimensional “Swallowtail” Cavity
35
Thermal Decomposition of Ethyl Formate behind the Reflected Shock Waves in the Temperature Range of 909-1258K
36
Kinetics of the Thermal Decomposition of Tetramethylsilane behind the Reflected Shock Waves in a Single Pulse Shock Tube (SPST) and Modeling Study
37
Numerical Simulation of Aluminum Dust Detonations with Different Product Phases
38
Effect of Smoked Foil Thickness and Location on Detonation Initiation
39
Mid-infrared Laser Absorption Diagnostics for Detonation Studies
40
Shock Wave – Boundary Layer Interaction in Reactive H2/O2 Mixture
41
Propagation of Sinusoidally-Corrugated Shock Fronts of Laser-Supported Detonations
42
On the Dynamic Detonation Parameters in Acetylene-Oxygen Mixtures with Varying Amount of Argon Dilution
43
Strong and Weak Ignition in 2H<sub>2</sub> + O<sub>2</sub> behind Reflected Shocks in Two-Dimensional Navier-Stokes Simulations with Detailed Chemistry
44
Velocity Fluctuations in the Interaction of Homogeneous, Isotropic Turbulence and a Detonation Wave
45
Deflagration-to-Detonation Transition of Methane-Oxygen Mixtures in Narrow Tubes
46
Influence of Methane on Ignition Delays of Hydrogen at Impulse Discharge from High Pressure Chamber
47
Experimental and Numerical Investigation of the HyShot II Flight Experiment
48
On the Hypersonic Analogy for Problems of Detonation Inside 3D Channels
49
Point Measurement of Detonation Wave Speed
50
Reflected Detonation Waves: Comparing Theory to Pressure and Heat Flux Measurements
51
Experiments in a Combustion-Driven Shock Tube with an Area Change
52
Rapid Opening Valve Assisted by Magnetic Force for a Diaphragmless Shock Tube
53
Improvement of a Diaphragmless Driver Section for a Small Diameter Shock Tube
54
Preliminary Experiment of the Drag Force Measurement by Using Strain Gauge in the Hypersonic Flow
55
A Numerical Investigation of the Flow through a New Fast Acting Valve for Diaphragmless Shock Tubes
56
Unsteady Drag Measurements for Hypersonic Shock Tunnel
57
Design and Commissioning of a New Lightweight Piston for the X3 Expansion Tube
58
High Mach Number Scramjet Test Flows in the X3 Expansion Tube
59
Investigation of Nozzle Starting Problem and Its Application to Construct a Supersonic Wind Tunnel
60
Gasdynamics/Mechanical Hybrid Sabot Separation Method Rectangular-Bore Ballistic Range
61
ISL Shock Tunnel Operation with Contoured Mach-4.5-6-8-10-Nozzles for Hypersonic Test Applications
62
Piezoelectric Pressure Microsensor Arrays for the Simultaneous Measurement of Shock Wave Amplitude, Velocity and Direction at a Point
63
Reddy Tube Driven Table-Top Hypersonic Shock Tunnel
64
Spectral Characteristics of Pitot Noise
65
Experimental Study of Moving Throat Plug in a Shock Tunnel
66
Analysis of a Quick-Acting Diaphragmless Shock Tube Driver
67
Supersonic Flow over a Rectangular Open Cavity: Effect of Length-to-Depth Ratio
68
LIF Visualization of a Supersonic Deep-Cavity Flow
69
Application of the Polymer Based Pressure Sensitive Paint for Qualitative and Quantitative Flow Visualisation in a Transonic Flow
70
Single-Plate-Imaging, Two-Wavelength Mach-Zehnder Interferometer
71
Background Oriented Schlieren Method Using Multi-scale Periodic Pattern
72
Orthogonal Projection Based Computationally Efficient Algorithm for Deflection Tomography in High Speed Flow Studies
73
NPLS Technique and Its Application on Complex Flow Field with Shock Waves
74
Toluene Laser-Induced Fluorescence (LIF) Imaging of Supersonic Flow within a Diverging Duct with Injectors in the Supersonic Region
75
Reconstruction of Unsteady and Axisymmetric Flow Field by Colored-Grid Background Oriented Schlieren (CGBOS) Technique
76
Four-Dimensional LICT Density Measurement of Unsteady Shock-Vortex Flow Discharged from Two Inclined and Cylindrical Holes Using High-Speed Camera
77
Ultrafast Time Response Pressure-Sensitive Paint for Unsteady Shock-Wave Research
78
Quantitative Density Measurement of the Interaction Field of Side Jet and Cross Flow by Colored-Grid Background Oriented Schlieren (CGBOS) Technique
79
Investigation on Flow Structures of Supersonic Isolator Flow
80
Visualization of Hypersonic Flat-Plate Boundary Layer in Shock Tunnel
81
Nonequilibrium and Rarefaction Effects in Hypersonic Multicomponent Viscous Shock Layers
82
Hypersonic High-Enthalpy Flow in a Leading-Edge Separation
83
About the “Camel Effect” on Heat Transfer to a Sphere at Hypersonic Flow Conditions
84
Side Jet/Cross Flow Interaction at Hypersonic Re-entry Conditions
85
Shock Standoff on Hemi-Spherical Bodies in Hypervelocity Flows
86
Global Pressure- and Temperature-Measurements in 1.27-m JAXA Hypersonic Wind Tunnel
87
Effects of Angle of Attack on the Behaviour of Imperfections in Thermal Protection Systems of Re-entry Vehicles
88
Hypersonic Interference Heating on Plates and Cones with Three-Dimensional Protuberances
89
Working towards Simulating Gas Giant Entry Radiation in an Expansion Tube
90
Numerical Predictions for Convective and Radiative Heating of a Spacecraft Entering a Planetary Atmosphere
91
Effect of the Shock Interaction on the Attitude Stability of the Toroidal Ballute for Reentry Vehicle
92
Effectiveness of Film Cooling over Large Angle Blunt Cones in High Speed Carbon Dioxide Flows
93
Tests of Hypersonic Inlet Oscillatory Flows in a Shock Tunnel
94
Emission Spectroscopy of a Mach Disk at Titan Atmospheric Entry Conditions
95
New Mode of Instability and Double Mach Reflection in Stationary Supersonic Gas Flow
96
Edney IV Interaction Studies at Mach 5
97
Diode-Laser-Based Driver Gas Detector for Hypersonic Shock Tunnels
98
Fluorescence Studies of Jet Mixing in a Hypersonic Flow
99
Turbulent Spot Initiation Rates in Boundary Layers in a Shock Tunnel
100
Experimental Measurement of Aerodynamic Heat Transfer due to Radiative Transmission in High Enthalpy Flow around a Re-entry Model
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