31st International Symposium on Shock Waves 1
Springer International Publishing
978-3-319-91019-2 (ISBN)
Chapter1.Aerodynamic Testing at Duplicated Hypersonic Flight Conditions with Hyper-Dragon.- Chapter2.Shock wave research: Remembrance of Professor I. I. Glass.- Chapter3.Legacy at T5.- Chapter4.Experimental studies of shock wave phenomena at the Ben Gurion University ? A Review.- Chapter5.Shock Compression Spectroscopy Under a Microscope.- Chapter6.Research on Shock-induced Aerothermodynamics for Future Planetary Explorations.- Chapter7.Kinetic shock Tubes: Recent developments for The study of homogeneous and heterogeneous chemical processs.- Chapter8.Structure and Unsteadiness of 3D Shock Wave / Turbulent Boundary Layer Interactions..- Chapter9.Propagation Behavior and Mitigation of Shock Wave along Water inside a Rectangular Tube.- Chapter10.Dust Lofting behind shock waves what is the dominate Lofting Mechanism.- Chapter11.Development of a fast running method for blast wave propagation.- Chapter12.On the Energy Exchange Mechanisms Controlling Blast and Fragment Evolution in a Responding Stone Pipe .- Chapter13.Interaction of a Blast Wave with a Material Interface.- Chapter14.Laboratory simulation of explosions using conical shock tubes.- Chapter15.Shock Tube Study of the Effect of Nitric Oxide Addition on Ignition Delay Times of n-Dodecane/Air Mixtures.- Chapter16.Ignition Delay Times of Methane and Hydrogen Highly Diluted in Carbon Dioxide.- Chapter17.A Study of the Chemiluminescence of *, *, 2* and 2* during the Oxidation of C2H2 behind Reflected Shock Waves .- Chapter18.A Study on Soot Formation Characteristics of a Gasoline Surrogate Fuel Using a Shock Tube.- Chapter19.Effect of Dimethyl Methylphosphonate (DMMP) Addition on H2, CH4, and C2H4 ignition Behind Reflected Shock Waves.- Chapter20.CO and H2O Time-histories in a Shock-heated H2S/CH4 Blend near Atmospheric Pressure.- Chapter21.Thermochemical nonequilibrium modeling of O2.- Chapter22.State-Resolved Transport Properties of Electronically Excited High-Temperature Flows behind Strong Shock Waves.- Chapter23.Oxygen Catalytic Recombination on Titanium Surface.- Chapter24.Computations of a Shock Layer Flow with a Vibrational-Specific Kinetics Model.- Chapter25.A One-dimensional Modeling of Seed-electron Generation and Electron Avalanche in Laser-supported Detonation.- Chapter26.PLIF-based concentration measurement of OH behind the blast wave emanating from an oxy-hydrogen detonation-driven shock tube.- Chapter27.Flame Propagation over the Heat Absorbing Substrate.- Chapter28.Propagation Mechanism of Detonations in Rough Walled Tube.- Chapter29.Effect of hydrodynamic instabilities on the development of hydrogen-air flame.- Chapter30.Characteristics of Crumpling Behavior of Graphene Oxide and Its Effects on Deflagration-to-Detonation Transition.- Chapter31.Detonation decay and flame propagation through a channel with porous walls.- Chapter32.Gas Flow with Stabilized Detonation in a Plane Channel.- Chapter33.Numerical Investigation on Vibrational Nonequilibrium Effect on ZND detonation model.- Chapter34.Stabilities of Rotating Detonation.- Chapter35.The influence of shock reflections on detonation re-initiation.- Chapter36.Experimental studies around shock tube for dynamic calibrations of high-frequency pressure transducers.- Chapter37.Effect of Imaging Blurring on 3D Computed Tomography of Chemiluminescence.- Chapter38.Time-Resolved Optical Flow of Supersonic Beveled Nozzles.- Chapter39.The Effect of Adaptive Sampling on Fluorescence Velocimetry Measurements in High-Speed Flows.- Chapter40.High-resolution background oriented schlieren technique for a laser-induced underwater shock wave.- Chapter41.Evaluation of the effect of an air plasma on the degradation of metallic coatings based on an analysis of the emission from the air behind the front of strong shock waves in the spectral range of 120 400 nm .- Chapter42.Application of NO Laser Induced Fluorescence in JF-10 Detonation-Driven Shock Tunnel.- Chapter43.Molecular Tagging Velocimetry of NH Fluorescence ina
| Erscheint lt. Verlag | 22.3.2019 |
|---|---|
| Zusatzinfo | XX, 1235 p. 787 illus., 540 illus. in color. In 2 volumes, not available separately. |
| Verlagsort | Cham |
| Sprache | englisch |
| Maße | 155 x 235 mm |
| Gewicht | 2229 g |
| Themenwelt | Technik ► Luft- / Raumfahrttechnik |
| Schlagworte | detonation technologies • Flow visualization • fluid- and aerodynamics • fundamental shockwave research • high-speed flow • ISSW31 proceedings • theoretical aspects of shockwaves |
| ISBN-10 | 3-319-91019-1 / 3319910191 |
| ISBN-13 | 978-3-319-91019-2 / 9783319910192 |
| Zustand | Neuware |
| Informationen gemäß Produktsicherheitsverordnung (GPSR) | |
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