ASYMPTOTIC THEORY OF THE BOLTZMANN EQUATION, II
Gas dynamics - asymptotic theory of boltzmann equation
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Gas dynamics - asymptotic theory of boltzmann equation
Gas dynamics - molecular beams and surface interactions
Gas dynamics - nonequilibrium statistical mechanics
Gas dynamics - shock wave thickness by monte carlo method
Gas dynamics - sound propagation according to kinetic theory of gases
Gas dynamics - characteristics of aerodynamic molecular beams
Gas dynamics - scattering of gas molecules on various surfaces
Gas dynamics - structure of strong shock waves in krook collision equation
Gas dynamics - revolving disks in study of interaction between molecules and surface
Gas dynamics - convergence & error estimation of iterative solution to nonlinear boltzmann equation
Gas dynamics - relaxation of gases towards continuum flow
This paper presents results of molecular dynamics computations of supersonic flow past a circular cylinder and past a flat plate perpendicular to a supersonic stream. The results are for Mach numbers of approximately 5 and 10, for several Knudsen numbers and several ratios of surface to free stream temperatures. A special feature of the computations is the use of relatively small numbers of particles in the molecular dynamics simulation, and an examination of the adequacy of using small numbers of particles to obtain physically useful results.
Gas dynamics - generalized validity of boltzmann equation for ionized gases
Gas dynamics - gas-surface interactions using modulated atomic beam
A theory is developed for a selection rule governing collisions in a particle simulation of rarefied gas-dynamic flows. The selection rule leads to an algorithmic form highly compatible with fine grain parallel decomposition, allowing for efficient utilization of supercomputers having vector or massively parallel single instruction multiple data architectures. A comparison of shock-wave profiles obtained using both the selection rule and Bird's direct simulation Monte Carlo (DSMC) method show excellent agreement. The equation on which the selection rule is based is shown to be directly related to the time-counter procedure in the DSMC method. The results of several example simulations of representative rarefied flows are presented, for which the number of particles used ranged from 10 to the 6th to 10 to the 7th demonstrating the greatly improved computational efficiency of the method.
Magnetic field of line current in transverse rarefied plasma stream
Radiative losses evaluated for all significant ions present in interplanetary gas from 4 to 215 radii - solar corona energy balance
Flow of rarefied gas over obstacles of small dimensions envisioned using network of fine wires