Solution of Falkner—Skan Equations for Hypersonic Flows

The results of the solution of the Falkner—Skan equation for compressible flows are obtained for the first time, in addition to those obtained by Hartree and Stewartson. The dependence of the viscous stress at the wall and the temperature gradient on the parameter is determined for different values...

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Veröffentlicht in:	Fluid dynamics 2020-07, Vol.55 (4), p.525-533
Hauptverfasser:	Lipatov, I. I., Ngo, K. T.
Format:	Artikel
Sprache:	eng
Schlagworte:	Classical and Continuum Physics Classical Mechanics Compressible flow Engineering Fluid Dynamics Fluid- and Aerodynamics Hypersonic flow Physics Physics and Astronomy Temperature gradients
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Beschreibung
Zusammenfassung:	The results of the solution of the Falkner—Skan equation for compressible flows are obtained for the first time, in addition to those obtained by Hartree and Stewartson. The dependence of the viscous stress at the wall and the temperature gradient on the parameter is determined for different values of the temperature factor g w .
ISSN:	0015-4628 1573-8507
DOI:	10.1134/S0015462820040072