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