A projectile that passes through a moving shock wave experiences drastic changes in the aerodynamic forces as it moves from a high-pressure region to a low-pressure region. These sudden changes in the forces are attributed to the wave structures produced by the projectile-shock-wave interaction ...
Shock Waves is dedicated to presenting and discussing new findings in fields associated with shock and detonation phenomena. Caters to physicists, engineers, ...
The present survey considers these conflicting perspectives, as well as results from different investigations which appear to be consistent. The present survey is presented in five parts. Discussed first are general features of shock wave interactions. Discussed second are test section configurations for ...
The largest expansion of shock wave physics certainly occurred during and after World War II, which created such new disciplines as hypersonic aerodynamics, nuclear explosions, detonics, exploding wires, rarefied gas dynamics, superaerodynamics, aerothermodynamics, magnetofluid dynamics, cosmic gas dynamics...
the incident shock wave at the inlet lip undergoes multiple reflections within the boundary layer of the domain wall, culminating in the formation of turbulent structures. The first reflected shock wave has the highest energy, exerting a significant impact on the boundary layer and the exit swirl ...
This book is aimed at practitioners and graduate students in aerodynamics who wish to familiarise themselves with all aspects of SBLI flows. It is a valuable resource for the specialist because it gathers experimental, computational and theoretical knowledge in one place. 展开 关键词:...
However, unlike the ordinary gasdynamic case, the solution inside rarefaction waves in magnetogasdynamics cannot be obtained directly and explicitly; indeed, ... TR Sekhar,VD Sharma - 《Nonlinear Analysis Real World Application》 被引量: 65发表: 2010年 Inviscid and viscous aerodynamics of dense gas...
Daniel T. Valentine, in Aerodynamics for Engineering Students (Sixth Edition), 2013 6.7.2 Shock Polar Although, in practice, data for plane shock waves are easily computed, numbers generally do not convey the trends and dependencies in the equations as well as a specialized plot can. The ...
In this section, the performance of aerodynamics and heat transfer in viscous supersonic and hypersonic flows is studied by FR-LBFS within the PyFR framework [39]. This includes simulating the double Mach reflection, viscous shock tube problem, shock wave/boundary layer interaction, supersonic comp...
An experimental study on the influence of on-board generated plasma on shock waves structures and blunt body aerodynamics in a supersonic flow is presented... R Miles,SO Macheret,L Martinelli,... 被引量: 0发表: 2001年 Numerical study of water mitigation effects on blast wave The mitigating...