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Tip-Vortex Investigation on a Rotating and Pitching Rotor Blade
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— ... and Pitching Rotor Blade Andreas Goerttler,∗ Johannes N. Braukmann,∗ Till Schwermer,† Anthony D. Gardner,† and Markus Raffel‡ DLR, ... › book
Experimentelle Untersuchung des dynamischen Strömungsabrisses ...books.google.com › books › about › Experimentelle_Unt...
books.google.com.ua
... des dynamischen Strömungsabrisses an einem Rotor mit axialer Zuströmung: Dynamic stall experiments on a rotor i axial inflow. Front Cover. Till Schwermer.
Experimentelle Untersuchung des dynamischen Strömungsabrisses an...
books.google.de
... einem Rotor mit axialer Zuströmung: 3 Tabellen, 129 Literaturstellen. Front Cover. Till Schwermer. DLR, Deutsches Zentrum für Luft- und Raumfahrt e.V.,
[PDF] Untersuchung junger Blattspitzenwirbel an einem Rotorteststand ...www.gala-ev.org › images › Beitraege › pdf
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· Johannes N Braukmann, Till Schwermer, C Christian Wolf. Deutsches Zentrum für Luft- und Raumfahrt e.V.Göttingen,.
The Tip Vortex System of a Four-Bladed Rotor in Dynamic ...Ingenta Connect
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von CC Wolf · · Zitiert von: 14 — Till Schwermer. Markus Raffel. Research Scientist. Research Scientist. Postgraduate Student. Research Scientist. Professor. German Aerospace Center, Göttingen ... von CC Wolf · · Zitiert von: 14 — Till Schwermer. Markus Raffel. Research Scientist. Research Scientist. Postgraduate Student. Research Scientist. Professor. German Aerospace Center, Göttingen ...
Development of a Rotor Test Facility for the Investigation of Dynamic...
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The flight envelope of modern helicopters is limited due to unsteady flow phenomena such as dynamic stall. Most investigations regarding this topic, both...
74th Annual Vertical Flight Society Forum and Technology Display
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... Johannes N. Braukmann, Wolfgang Stauber, Till Schwermer, Markus Raffel Three-Component Reverse Flow Measurements on a Mach-Scale Rotor at High ...
AHS International 74 th Annual Forum & Technology Display. May ,...
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· ... Four-Bladed Rotor in Dynamic Stall Conditions (206) C. Christian Wolf*, Johannes N. Braukmann, Wolfgang Stauber, Till Schwermer, Markus ...
Forschungsbericht / Deutsches Zentrum für Luft- und Raumfahrt: DLR FB...
katalog.slub-dresden.de
Schwermer, Till [ Autor/In ] 2018, 14: Experimentelle Untersuchung des dynamischen Strömungsabrisses an einem Rotor mit axialer Zuströmung Till Schwermer, Deutsches Zentrum für Luft- und Raumfahrt, Institut für Aerodynamik und Strömungstechnik, Göttingen Köln, DLR, Deutsches Zentrum für Luft- …
electronic library - The Tip Vortex System of a Four-Bladed Rotor in...
elib.dlr.de
Deutsches Zentrum für Luft- und Raumfahrt e.V., eLib - DLR electronic library
Differential infrared thermography for boundary layer transition ...www.infona.pl › resource
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... thermography for boundary layer transition detection on pitching rotor blade models. Markus Raffel, Christoph B. Merz, Till Schwermer, Kai Richter.
Journal of the American Helicopter Society Latest Journal Impact IF ...academic-accelerator.com › Impact-of-Journal › Jou...
academic-accelerator.com
A Novel Experiment to Understand the Dynamic Stall Phenomenon in Rotor Axial Flight · Till Schwermer · Anthony Donald Gardner · Markus Raffel.
Numerical Investigations of Dynamic Stall on a Rotor with ...EBSCO Information Services
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von J Letzgus · · Zitiert von: 29 — Till Schwermer. Research Assistant. Senior Scientist. Research Assistant. Institute of Aerodynamics and Gas Dynamics. German Aerospace Center (DLR). University ... von J Letzgus · · Zitiert von: 29 — Till Schwermer. Research Assistant. Senior Scientist. Research Assistant. Institute of Aerodynamics and Gas Dynamics. German Aerospace Center (DLR). University ...
On the Effect of Rotational Forces on Rotor Blade ...Aerospace Research Central
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von A Weiss · · Zitiert von: 31 — Till Schwermer. ‡. Christian Klein. §. Markus Raffel. ¶. German Aerospace Center (DLR) ... ‡Research Scientist, Department Helicopters, ,. von A Weiss · · Zitiert von: 31 — Till Schwermer. ‡. Christian Klein. §. Markus Raffel. ¶. German Aerospace Center (DLR) ... ‡Research Scientist, Department Helicopters, ,.
Numerical Investigations of Dynamic Stall on a Rotor with Cyclic...
www.semanticscholar.org
... Pitch Control}, author={Johannes Letzgus and Anthony Donald Gardner and Till Schwermer and Manuel Ke{\ss}ler and Ewald Kr{\"a}mer}, year={2019} }.
[PDF] Single-shot pressure-sensitive paint lifetime measurements on...
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Development of an innovative double-swept rotorblade tip for the rotor test facility Goettingen · Martin Michael Mueller, Till Schwermer, Holger Mai, Christian ...
[PDF] Development of an innovative double-swept rotorblade tip for...
www.semanticscholar.org
... double-swept rotorblade tip for the rotor test facility Goettingen}, author={M. Mueller and Till Schwermer and H. Mai and Christian Stieg}, year={2018} }.
[PDF] The effect of vortex generators on the flow around a circular...
www.semanticscholar.org
Benjamin Heine, Till Schwermer, Markus Raffel; Published The effect of circular low-profile vortex generators for rotorcraft application has been ...
[PDF] Dynamic Stall on a Pitching Double-Swept Rotor Blade Tip |...
www.semanticscholar.org
Dynamic stall is experimentally and numerically investigated on a pitching double-swept helicopter rotor blade tip. The aerodynamic and structural design of...
Article - A Novel Experiment to Understand the Dynamic Stall ...
www.scilit.net
— A Novel Experiment to Understand the Dynamic Stall Phenomenon in Rotor Axial Flight. Till Schwermer,. Anthony D. Gardner. , Markus Raffel. › article
Development of a Rotor Test Facility for the Investigation of Dynamic ...elib.dlr.de › ...
elib.dlr.de
Schwermer, Till, Till.Schwermer (at) dlr.de, https://orcid.org Richter, Kai, Kai.Richter (at) dlr.de. Raffel, Markus, Markus.
Development of an innovative double-swept rotor blade tip for the ...elib.dlr.de › ...
elib.dlr.de
Schwermer, Till, Till.Schwermer (at) dlr.de. Mai, Holger, Holger.Mai (at) dlr.de. Stieg, Christian, Christian.stieg (at) dlr.de ...
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