A Study of the Liquefaction Shock Wave Structure
نویسنده
چکیده
The system of shock wave-induced vapor condensation in uids of large heat capacity has been investigated theoretically. The wave structure is governed by diierences in the time scales associated with various relaxation mechanisms and their coupling to the macroscopic ow. In the low to moderate Mach number range, the viscous and heat-conducting forces are localized within a discontinuous forerunner wave, while the slower nucleation and droplet growth processes are resolved inside a trailing condensation wave. A time-dependent analysis of the uid motion is required because the phase transition can occur too slowly for the system to reach a steady state on the laboratory time scale. In the high Mach number regime, a steady-state motion is rapidly attained, but the analysis requires a simultaneous treatment of nucleation, viscosity, and heat conduction. It appears that instability mechanisms similar to the ones found in ZND detonation waves are responsible for the shock-front irregularities observed in high Mach-number ows. Based on the rapidity of the supersaturating shock compression and the time delay of nucleation, it is anticipated that metastable states near the vapor spinodal are attainable, especially at high temperatures.
منابع مشابه
Evaluating the Liquefaction Potential of Soil in the South and Southeast of Tehran based on the Shear Wave Velocity through Empirical Relationships
The liquefaction resistance of soil can be evaluated using laboratory tests such as cyclic simple shear, cyclic triaxial, cyclic torsional shear as well as field methods like Standard Penetration Test (SPT), Cone Penetration Test (CPT) and Shear Wave Velocity (Vs). In this regard, this study attempts to compare the results of the SPT based on the simplified procedure proposed by Seed and Idriss...
متن کاملOscillation Control of Aircraft Shock Absorber Subsystem Using Intelligent Active Performance and Optimized Classical Techniques Under Sine Wave Runway Excitation (TECHNICAL NOTE)
This paper describes third aircraft model with 2 degrees of freedom. The aim of this study is to develop a mathematical model for investigation of adoptable landing gear vibration behavior and to design Proportional Integration Derivative (PID) classical techniques for control of active hydraulic nonlinear actuator. The parameters of controller and suspension system are adjusted according to be...
متن کاملThe effect of three sessions shock wave therapy on spasticity and range of motion of lower limb in stroke patients
Background: Spasticity is a common motor impairment in patients with stroke that not only has a negative impact on the patient’s quality of life but also has high economic burdens for society. Recently the application of shock wave therapy has attracted considerable attention as a safe and effective method in treatment of spasticity. The objective of the present study was to investigate the eff...
متن کاملبستههای نسوخته گازی در تراکهای با ساختار نامنظم (علمی-پژوهشی)
Abstract A two-dimensional numerical simulation is performed in the present work to study the structure of a detonation wave in high activation energy mixtures, which are characterized by their turbulent reaction zone structure and unreacted pockets. The process of transverse wave and triple point collision with the channel walls, formation and consumption mechanism of unburnt gas pockets is e...
متن کاملAn Optical Measurement System to Measure Velocity and Provide Shock Wave Pressure Diagrams
This paper introduces an optical measurement system for shock wave characteristics. The system works by mountinga metal plate attached to spring mounts against the shock wavefront. This set is sealed and can plot the shock wave pressure diagram by measuring plate's displacement, radiation and changing the reflection of light during shock wave conflict, and converting these optical data to volta...
متن کامل