Effect of forward-facing steps on boundary layer transition at a subsonic Mach number

Costantini, Marco and Risius, Steffen and Klein, Christian and Kühn, Winfried (2014) Effect of forward-facing steps on boundary layer transition at a subsonic Mach number. 19. DGLR-Fachsymposium der STAB, 2014-11-04 - 2014-11-05, München, Deutschland.

Full text not available from this repository.

Official URL: http://www.stab2014.tum.de/

Item URL in elib:

https://elib.dlr.de/89793/

Document Type:

Conference or Workshop Item (Speech)

Title:

Effect of forward-facing steps on boundary layer transition at a subsonic Mach number

Authors:

Authors	Institution or Email of Authors	Author's ORCID iD	ORCID Put Code
Costantini, Marco	UNSPECIFIED	https://orcid.org/0000-0003-0642-0199	134173716
Risius, Steffen	UNSPECIFIED	UNSPECIFIED	UNSPECIFIED
Klein, Christian	UNSPECIFIED	https://orcid.org/0000-0001-7592-6922	UNSPECIFIED
Kühn, Winfried	Airbus Operations SAS	UNSPECIFIED	UNSPECIFIED

Date:

2014

Refereed publication:

Yes

Open Access:

Gold Open Access:

In SCOPUS:

In ISI Web of Science:

Page Range:

pp. 68-69

Series Name:

Jahresbericht 2014

Status:

Published

Keywords:

Boundary layer transition, forward-facing steps, Temperature-Sensitive Paint

Event Title:

19. DGLR-Fachsymposium der STAB

Event Location:

München, Deutschland

Event Type:

national Conference

Event Start Date:

4 November 2014

Event End Date:

5 November 2014

HGF - Research field:

Aeronautics, Space and Transport

HGF - Program:

Aeronautics

HGF - Program Themes:

fixed-wing aircraft

DLR - Research area:

Aeronautics

DLR - Program:

L AR - Aircraft Research

DLR - Research theme (Project):

L - Simulation and Validation (old)

Location:

Göttingen

Institutes and Institutions:

Institute of Aerodynamics and Flow Technology > Experimental Methods

Deposited By:

Micknaus, Ilka

Deposited On:

24 Nov 2014 11:48

Last Modified:

24 Apr 2024 19:55

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