Shock Wave Reflection PhenomenaSpringer Science & Business Media, 28 באוג׳ 2007 - 342 עמודים This book is a comprehensive state-of-the-knowledge summation of shock wave reflection phenomena from a phenomenological point of view. It includes a thorough introduction to oblique shock wave reflections, dealing with both regular and Mach types. It also covers in detail the corresponding two- and three-shock theories. The book moves on to describe reflection phenomena in a variety of flow types, as well as providing the resolution of the Neumann paradox. |
תוכן
1 | |
Near the Reflection Point of a Regular Reflection | 21 |
Shock Wave Reflections in Steady Flows | 39 |
Shock Wave Reflections in Pseudosteady Flows | 135 |
Reflection Domains | 233 |
Shock Wave Reflections in Unsteady Flows | 247 |
Source List | 307 |
338 | |
מהדורות אחרות - הצג הכל
מונחים וביטויים נפוצים
additional analytical assumed assumption Ben-Dor boundary layer calculated combination concave criterion curved cylindrical decreases dependence detachment domain edge effects equations exist experimental experimental results experiments fact Figure flow field Fluid Mech frame given height hence incident shock wave increases indicates initial InMR inside interaction intersects length Mach reflection Mach stem mentioned Neumann Note oblique shock wave obtained perfect phenomenon polar possible predictions presented pressure pseudosteady reached reference reflected shock wave reflecting surface reflecting wedge reflection point region regular reflection respectively roughness RR wave configuration Schematic illustration second triple point shock wave reflection showed shown in Fig situation slipstream solution steady flows straight supersonic Takayama theoretically three-shock theory tion Tohoku University transition line transition wedge angle triple point Type various von Neumann wave configuration weak wedge angle
קטעים בולטים
עמוד 334 - Tabular and Graphical Solutions of Regular and Mach Reflections in Pseudo-Stationary Frozen and Vibrational-Equilibrium Flows", Univ.