The shock-wave structure for arbitrary Prandtl numbers and high Mach numbers

Details The shock-wave structure for arbitrary Prandtl numbers and high Mach numbers The shock-wave structure for arbitrary Prandtl numbers and high Mach numbers

Jul 1985

adsabs.harvard.edu/cgi-bin/nph-data_query?bibcode=1985ap%26ss.113..289k&link_type=abstract

Astrophysics and Space Science (ISSN 0004-640X), vol. 113, no. 2, July 1985, p. 289-301.

Astronomy and Astrophysics

Astrophysics

1

Mach Number, Prandtl Number, Shock Waves, Enthalpy, Flow Velocity, Monatomic Gases, Pressure Distribution, Viscosity

Scientific paper

By use of a modified law of viscosity of the form μ = Tn,
where n is a given function of M, an analytical solution is obtained to
the problem of strong shock waves. These analytical results agree very
well with results obtained by using Boltzmann equation to the same
problem.

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