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An Integral Method for Two-Dimensional, Compressible, Adiabatic, Turbulent Boundary Layers

Stock, H.W. (1998) An Integral Method for Two-Dimensional, Compressible, Adiabatic, Turbulent Boundary Layers. DLR-Interner Bericht. 129-98/10, 21 S.

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Abstract

An integral method is proposed to calculate adiabatic, turbulent boundary layers in compressible flow. For the description of the velocity profiles the Coles formulation is applied. The compressible effects are taken into account by the Stewartson-Illingworth transformation. Turbulence is modeled via the use of the entrainment concept. In order to cope with history effects of the boundary layer the lag-entrainment idea is adopted. The quality of the results of the integral method is documented for three different flow cases. The first tow cases are experiments in a low speed - and in a high supersonic flow, respectively. The third case uses Navier-Stokes results for an airfoil in subsonic, compressible flow for comparison.

Item URL in elib:https://elib.dlr.de/36629/
Document Type:Monograph (DLR-Interner Bericht)
Additional Information: LIDO-Berichtsjahr=1998,
Title:An Integral Method for Two-Dimensional, Compressible, Adiabatic, Turbulent Boundary Layers
Authors:
AuthorsInstitution or Email of AuthorsAuthors ORCID iD
Stock, H.W.UNSPECIFIEDUNSPECIFIED
Date:1998
Open Access:No
Gold Open Access:No
In SCOPUS:No
In ISI Web of Science:No
Number of Pages:21
Status:Published
Keywords:2D Compressible Turbulent Boundary Layer, Integral Method
HGF - Research field:UNSPECIFIED
HGF - Program:Aeronautics
HGF - Program Themes:other
DLR - Research area:UNSPECIFIED
DLR - Program:L ST - Starrflüglertechnologien
DLR - Research theme (Project):L - Concepts & Integration (old)
Location: Köln-Porz , Braunschweig , Göttingen
Institutes and Institutions:Institute of Aerodynamics and Flow Technology > Institut für Entwurfsaerodynamik
Deposited By: DLR-Beauftragter, elib
Deposited On:03 Apr 2006
Last Modified:27 Apr 2009 10:06

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