Direct numerical simulation of transition in supersonic boundary layers: oblique breakdown

H. Fasel; A. Thumm; H. Bestek

Direct numerical simulation of transition in supersonic boundary layers: oblique breakdown

H. Fasel, A. Thumm, H. Bestek

Aerospace and Mechanical Engineering

Research output: Chapter in Book/Report/Conference proceeding › Conference contribution

101 Scopus citations

Abstract

Laminar-turbulent transition phenomena in compressible flat-plate boundary layers are investigated by direct numerical simulations using the complete Navier-Stokes equations for three-dimensional compressible flows. The numerical method allows for investigations of spatially developing, three-dimensional disturbance waves in a growing two-dimensional boundary layer. In this paper, results from simulations for two different types of breakdown to turbulence in a flat-plate boundary layer at M∞ =1.6 are presented.

Original language	English (US)
Title of host publication	Transitional and Turbulent Compressible Flows - 1993
Publisher	Publ by ASME
Pages	77-92
Number of pages	16
ISBN (Print)	0791809595
State	Published - 1993
Event	Fluids Engineering Conference - Washington, DC, USA Duration: Jun 20 1993 → Jun 24 1993

Publication series

Name	American Society of Mechanical Engineers, Fluids Engineering Division (Publication) FED
Volume	151

Other

Other	Fluids Engineering Conference
City	Washington, DC, USA
Period	6/20/93 → 6/24/93

ASJC Scopus subject areas

General Engineering

Cite this

Direct numerical simulation of transition in supersonic boundary layers: oblique breakdown. / Fasel, H.; Thumm, A.; Bestek, H.
Transitional and Turbulent Compressible Flows - 1993. Publ by ASME, 1993. p. 77-92 (American Society of Mechanical Engineers, Fluids Engineering Division (Publication) FED; Vol. 151).

Research output: Chapter in Book/Report/Conference proceeding › Conference contribution

Fasel, H, Thumm, A & Bestek, H 1993, Direct numerical simulation of transition in supersonic boundary layers: oblique breakdown. in Transitional and Turbulent Compressible Flows - 1993. American Society of Mechanical Engineers, Fluids Engineering Division (Publication) FED, vol. 151, Publ by ASME, pp. 77-92, Fluids Engineering Conference, Washington, DC, USA, 6/20/93.

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Direct numerical simulation of transition in supersonic boundary layers: oblique breakdown

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