Theory of Tollmien-Schlichting waves is studied in transonic flow regime. In the matter of linear analysis the dispersion relation for normal modes of instability is obtained. In the matter of nonlinear analysis an equation for amplitude of Tollmien-Schlichting waves is derived. Furthermore the supersonic limit is inspected

Linear and Weakly Non-linear Analysis of the Stability of the Boundary Layer in Transonic flow

Mazzetto, Alberto
2014/2015

Abstract

Theory of Tollmien-Schlichting waves is studied in transonic flow regime. In the matter of linear analysis the dispersion relation for normal modes of instability is obtained. In the matter of nonlinear analysis an equation for amplitude of Tollmien-Schlichting waves is derived. Furthermore the supersonic limit is inspected
2014-05
95
Boundary layer, stability, transonic
Turolla, Roberto
Ruban, Anatoly
Lauree magistrali
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Utilizza questo identificativo per citare o creare un link a questo documento: https://hdl.handle.net/20.500.12608/18514