Automatic Transition Prediction for High-Lift Configurations using a Hybrid CFD Code

Krumbein, Andreas and Krimmelbein, Normann (2008) Automatic Transition Prediction for High-Lift Configurations using a Hybrid CFD Code. 46th AIAA Aerospace Sciences Meeting and Exhibit, 2008-01-07 - 2008-01-10, Reno, NV (USA).

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Item URL in elib:

https://elib.dlr.de/52812/

Document Type:

Conference or Workshop Item (Speech, Paper)

Title:

Automatic Transition Prediction for High-Lift Configurations using a Hybrid CFD Code

Authors:

Authors	Institution or Email of Authors	Author's ORCID iD	ORCID Put Code
Krumbein, Andreas	UNSPECIFIED	UNSPECIFIED	UNSPECIFIED
Krimmelbein, Normann	Technische Universität Braunschweig, Institut für Strömungsmechanik	UNSPECIFIED	UNSPECIFIED

Date:

9 January 2008

Refereed publication:

Open Access:

Gold Open Access:

In SCOPUS:

In ISI Web of Science:

Editors:

Editors	Email	Editor's ORCID iD	ORCID Put Code
American Institute of Aeronautics and Astronautics, AIAA	UNSPECIFIED	UNSPECIFIED	UNSPECIFIED

Status:

Published

Keywords:

transition, automatic transition prediction, Reynolds averaged Navier-Stokes, DLR TAU code, 3d aircraft, wing body, high lift, local linear stability code, laminar boundary layer code

Event Title:

46th AIAA Aerospace Sciences Meeting and Exhibit

Event Location:

Reno, NV (USA)

Event Type:

international Conference

Event Start Date:

7 January 2008

Event End Date:

10 January 2008

Organizer:

AIAA

HGF - Research field:

Aeronautics, Space and Transport

HGF - Program:

Aeronautics

HGF - Program Themes:

Aircraft Research (old)

DLR - Research area:

Aeronautics

DLR - Program:

L AR - Aircraft Research

DLR - Research theme (Project):

L - Concepts & Integration (old)

Location:

Göttingen

Institutes and Institutions:

Institute of Aerodynamics and Flow Technology > CASE

Deposited By:

Krumbein, Dr.-Ing. Andreas

Deposited On:

16 Jan 2008

Last Modified:

24 Apr 2024 19:16

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