Comparison of different fidelity aerodynamic solvers on the IEA 10 MW turbine including novel tip extension geometries
- Location
-
Deutsche Nationalbibliothek Frankfurt am Main
- Extent
-
Online-Ressource
- Language
-
Englisch
- Bibliographic citation
-
In: Journal of Physics: Conference Series (2265:3) - Bristol : IOP - Art.-Id. 032002
- Event
-
Veröffentlichung
- (where)
-
Berlin
- (who)
-
Technische Universität Berlin
- (when)
-
2022
- Creator
-
Behrens de Luna, Robert
Marten, David
Barlas, T.
Horcas, S. G.
Ramos-García, N.
Li, A.
Paschereit, Christian Oliver
- DOI
-
10.14279/depositonce-15851
- Handle
-
11303/17072
- URN
-
urn:nbn:de:101:1-2022061502022607374475
- Rights
-
Der Zugriff auf das Objekt ist unbeschränkt möglich.
- Last update
-
25.03.2025, 1:56 PM CET
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
- Behrens de Luna, Robert
- Marten, David
- Barlas, T.
- Horcas, S. G.
- Ramos-García, N.
- Li, A.
- Paschereit, Christian Oliver
- Technische Universität Berlin
Time of origin
- 2022
Other Objects (12)
Robust multilevel elliptic problem solvers for anisotropic unstructured geometries
Aerodynamic optimization of turbine airfoils using multi-fidelity surrogate models
Hydrodynamic coupling of multi-fidelity solvers in REEF3D with application to ship-induced wave modelling
Optimization and coupling strategies for codes of different fidelity to automate an aerodynamic compressor design process
Application of Computational Aerodynamic Analysis and Optimization in a Multi-Fidelity Distributed Overall Aircraft Design System
IEA-Kongreß
Fidelity - Innocence
![[Treue; Fidelity]](https://iiif.deutsche-digitale-bibliothek.de/image/2/478d5461-c8c6-4991-9492-7ec03210ff15/full/!306,450/0/default.jpg)
[Treue; Fidelity]
Fidelity-Investmentfonds
Fidelity-Investmentfonds
Development of a mid fidelity aerodynamic analysis approach in the conceptual design of a tandem tiltwing eVTOL
Approach for the Aerodynamic Optimization of the Twist Distribution of Arbitrary Wing Geometries on Conceptual Aircraft Design Level
Robust multilevel elliptic problem solvers for anisotropic unstructured geometries
Aerodynamic optimization of turbine airfoils using multi-fidelity surrogate models
Hydrodynamic coupling of multi-fidelity solvers in REEF3D with application to ship-induced wave modelling
Optimization and coupling strategies for codes of different fidelity to automate an aerodynamic compressor design process
Application of Computational Aerodynamic Analysis and Optimization in a Multi-Fidelity Distributed Overall Aircraft Design System
IEA-Kongreß
Fidelity - Innocence
[Treue; Fidelity]
Fidelity-Investmentfonds
Fidelity-Investmentfonds
Development of a mid fidelity aerodynamic analysis approach in the conceptual design of a tandem tiltwing eVTOL
Approach for the Aerodynamic Optimization of the Twist Distribution of Arbitrary Wing Geometries on Conceptual Aircraft Design Level
Robust multilevel elliptic problem solvers for anisotropic unstructured geometries
Aerodynamic optimization of turbine airfoils using multi-fidelity surrogate models
Hydrodynamic coupling of multi-fidelity solvers in REEF3D with application to ship-induced wave modelling
Optimization and coupling strategies for codes of different fidelity to automate an aerodynamic compressor design process
Application of Computational Aerodynamic Analysis and Optimization in a Multi-Fidelity Distributed Overall Aircraft Design System
IEA-Kongreß
Fidelity - Innocence
[Treue; Fidelity]
Fidelity-Investmentfonds
Fidelity-Investmentfonds
Development of a mid fidelity aerodynamic analysis approach in the conceptual design of a tandem tiltwing eVTOL