A finite-element transonic potential flow solver with an embedded wake approach for aircraft conceptual design
- Alternative title
-
Ein Finite-Elemente transsonischer Potentialströmungslöser mit eingebettetem Wirbelschleppenansatz für den Flugzeug-Konzeptentwurf
- Location
-
Deutsche Nationalbibliothek Frankfurt am Main
- Extent
-
Online-Ressource
- Language
-
Englisch
- Notes
-
München, Technische Universität München, Dissertation, 2022
- Keyword
-
Design
- Event
-
Veröffentlichung
- (where)
-
München
- (who)
-
Universitätsbibliothek der TU München
- (when)
-
2022
- Creator
-
López Canalejo, Iñigo Pablo
- Contributor
- URN
-
urn:nbn:de:bvb:91-diss-20220505-1633175-1-3
- Rights
-
Der Zugriff auf das Objekt ist unbeschränkt möglich.
- Last update
-
15.08.2025, 7:40 AM CEST
Data provider
This object is provided by:
Deutsche Nationalbibliothek. If you have any questions about the object, please contact the data provider.
Deutsche Nationalbibliothek. If you have any questions about the object, please contact the data provider.
Associated
- López Canalejo, Iñigo Pablo
- Bletzinger, Kai-Uwe
- Breitsamter, Christian W. M.
- Rossi, Riccardo
- Universitätsbibliothek der TU München
Time of origin
- 2022
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Commercial aircraft wake vortices
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Unsteady shock front waviness in shock-buffet of transonic aircraft
Towards extending the aircraft flight envelope by mitigating transonic airfoil buffet
Towards extending the aircraft flight envelope by mitigating transonic airfoil buffet
Experimental investigation on the turbulent wake flow in fully established transonic buffet conditions
Wake vortices of landing aircraft : 4 Tabellen
Comparing aircraft wake turbulence with induced power calculations
Grey area in embedded wall-modelled LES on a transonic nacelle-aircraft configuration
The curled wake model: A three-dimensional and extremely fast steady-state wake solver for wind plant flows
Particle Image Velocimetry Measurements in Accelerated, Transonic Wake Flows
Commercial aircraft wake vortices
Wake vortices of landing aircraft
Wake vortices of landing aircraft
Unsteady shock front waviness in shock-buffet of transonic aircraft
Towards extending the aircraft flight envelope by mitigating transonic airfoil buffet
Towards extending the aircraft flight envelope by mitigating transonic airfoil buffet
Experimental investigation on the turbulent wake flow in fully established transonic buffet conditions
Wake vortices of landing aircraft : 4 Tabellen
Comparing aircraft wake turbulence with induced power calculations
Grey area in embedded wall-modelled LES on a transonic nacelle-aircraft configuration