A model of Fermi acceleration at shock fronts with an application to the earth's bow shock.
Model of Fermi acceleration at shock front developed and applied to Earth bow shock
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Model of Fermi acceleration at shock front developed and applied to Earth bow shock
Shock waves and shock wave structure in magnetohydrodynamics
Electromagnetic shock tube - linear discharge tube for generating strong shocks in air by high voltage spark
Shock front shape perturbations due to boundary layer effects and shock tube and piston imperfections
Shock tube studies of physical and chemical changes of carbon dioxide molecules in flow behind shock wave
Microwave and optical diagnostic techniques applied to high enthalpy shock tube and shock tunnel plasma flows
Slingshot device for high-velocity shock testing analyzed for impact delivery, shock pulse, and g-level
High enthalpy shock tube and nozzle gas flows for incident shock Mach numbers analyzed for laminar boundary layers and boundary layer transitions
Coherent precipitates effect on explosive shock hardening of pure nickel and Inconel alloy sandwich assemblies determined from simultaneous shock loading at specific pressures
Radiative cooling of shock heated air in cylindrical shock tubes, calculating enthalpy profiles for nonadiabatic air flow
Shock induced exothermic reactions on boundary layer transition in shock tube, investigating free stream thermal energy release effects
Carbon dioxide IR radiation measurements of duration of constant reflected shock temperature in overtailored shock tunnel
The principles, theoretical flow equations, calculation techniques, limitations and practical performance characteristics of basic and high performance shock tubes and shock tunnels are presented. Selected operating curves are included.
Abrupt and prolonged enhancements in the intensities of 100 to approximately 2000 keV nucleon protons and alpha particles observed in interplanetary space are interpreted as particle populations confined between an interplanetary shock front and a magnetic field discontinuity. Prominent intensity spikes observed only below approximately 400 keV per charge for both protons and alpha particles several hours behind the shock front suggest that some fraction of the confined particles is accelerated by an energy per charge dependent process.
Development in the modeling and simulation of shock and vibration phenomena are considered. Predicting the noise exposure of payloads in the space shuttle, prediction for step-stress fatigue, pyrotechnique shock simulation using metal-to-metal impact, and prediction of fragment velocities and trajectories are among the topics covered.
The interaction of a planar shock wave with one or more vortexes is computed using a pseudospectral method and a finite difference method. The development of the spectral method is emphasized. In both methods the shock wave is fitted as a boundary of the computational domain. The results show good agreement between both computational methods. The spectral method is, however, restricted to smaller time steps and requires use of filtering techniques.
The interaction of a shock wave with a hot spot, a single vortex and a vortex street is studied within the framework of the two dimensional compressible Euler equations. The numerical results obtained by the pseudospectral method and the finite difference MacCormack method are compared. In both the methods the shock wave is fitted as a boundary of the computational domain.
More precisely, calling xi the reciprocal of the Reynolds number based on the shock wave curvature radius, the xi terms of the first order are systematically taken into account. The most important result is a system of formulas giving a correction of order xi for the various RANKINE-HUGONIOT conditions. The suggested formulas may for instance have to be used instead of the conventional ones to evaluate the loss of the total pressure across the detached shock wave which is found at the nose of a very small probe in supersonic flow.