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Unsteady boundary layer transition detection by automated analysis of hot film data

Goerttler, Andreas and Gardner, Anthony and Richter, Kai (2016) Unsteady boundary layer transition detection by automated analysis of hot film data. 20. DGLR-Fachsymposium der STAB, 08.-09. Nov. 2016, Braunschweig, Deutschland.

Full text not available from this repository.

Official URL: https://www.tu-braunschweig.de/stab2016

Abstract

Serveral automated algorithms are implemented to examine the transitional behavior of the pitching airfoil DSA-9A. The state of the art method to detect unsteady boundary layer transition with experimental hot film data is a manual approach. Therefore to reduce the investigation time an improve the data quality an automated detection has been created. In the most cases the computation time of the unsteady boundary layer detection is almost two orders of magnitude faster compared to manual extraction. Several algorithms will be discussed in this paper of which an algorithm utilizing the skewness produces the best results in a robust implementation.

Item URL in elib:https://elib.dlr.de/110617/
Document Type:Conference or Workshop Item (Speech)
Title:Unsteady boundary layer transition detection by automated analysis of hot film data
Authors:
AuthorsInstitution or Email of AuthorsAuthors ORCID iD
Goerttler, Andreasandreas.goerttler (at) dlr.deUNSPECIFIED
Gardner, Anthonyanthony.gardner (at) dlr.dehttps://orcid.org/0000-0002-1176-3447
Richter, KaiKai.Richter (at) dlr.deUNSPECIFIED
Date:2016
Refereed publication:No
Open Access:No
Gold Open Access:No
In SCOPUS:No
In ISI Web of Science:No
Status:Published
Keywords:algorithm, unsteady boundary layer Transition, hot film, automatic analysis
Event Title:20. DGLR-Fachsymposium der STAB
Event Location:Braunschweig, Deutschland
Event Type:national Conference
Event Dates:08.-09. Nov. 2016
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
Location: Göttingen
Institutes and Institutions:Institute of Aerodynamics and Flow Technology > Helicopters
Institute of Aerodynamics and Flow Technology > High Speed Configurations
Deposited By: Bachmann, Barbara
Deposited On:12 Jan 2017 16:13
Last Modified:12 Jan 2017 16:13

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