Consideration is given to model of the hypersonic transitional flow regime
over space antennae. Model was used for studying aerodynamic characteristics
of parabolic antenna witch real wire netting elements were simulated by
perforated plates. Model of non-equilibrium flows description can give
as opportunity to determine and some parameters in a flow field. Model
of Low Density Gas Flow in Perforated Bounds has been developed for transparent
surface when Direct simulation Monte Carlo method loses there efficient.
Numerical results of studying aerodynamic characteristics and parameters
in a flow field are presented.
AERODYNAMIC OF NETTING SPACE ANTENNAE AND FLOW
Report on 13 International School "Models Of Continuum
Mechanics " St.Petersburg June 25 - 30, 1995,
Programme: Institute of Theoretical
and Applied Mechanics, SB, RAS, Novosibirsk, 1995, p.8.
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