Hochschulschrift
The transonic compressor with inlet guide vane asymmetry for aerodynamic mistuning: effects on aerodynamics and aeroelasticity : = Der Transsonikverdichter mit Eintrittsleitradschaufelasymmetrie zum aerodynamischen Mistuning: Auswirkungen auf Aerodynamik und Aeroelastizität
- Alternative title
-
Der Transsonikverdichter mit Eintrittsleitradschaufelasymmetrie zum aerodynamischen Mistuning: Auswirkungen auf Aerodynamik und Aeroelastizität
- Location
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Deutsche Nationalbibliothek Frankfurt am Main
- ISBN
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9783844090512
3844090517
- Dimensions
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21 cm, 244 g
- Extent
-
xxiv, 153 Seiten
- Language
-
Englisch
- Notes
-
Illustrationen
Technische Universität Darmstadt, Dissertation, 2023
- Bibliographic citation
-
Forschungsberichte aus dem Institut für Gasturbinen, Luft- und Raumfahrtantriebe / Technische Universität Darmstadt ; Band 21
- Keyword
-
Flugtriebwerk
Transsonischer Verdichter
Aerodynamik
Aeroelastizität
Leitrad
Frequenzverstimmung
Schaufelschwingung
Schaufelverstellung
Prüfstand
Aerodynamik
Flugtriebwerk
Aeroelastizität
Fluid-Struktur-Wechselwirkung
Verdichter
Rotor
- Event
-
Veröffentlichung
- (where)
-
Düren
- (who)
-
Shaker Verlag
- (when)
-
2023
- Creator
- Contributor
- Table of contents
- Rights
-
Bei diesem Objekt liegt nur das Inhaltsverzeichnis digital vor. Der Zugriff darauf ist unbeschränkt möglich.
- Last update
-
11.03.2025, 11:48 AM 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.
Object type
- Hochschulschrift
Associated
- Franke, Daniel
- Shaker Verlag
- Shaker Verlag
Time of origin
- 2023
Other Objects (12)
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Aerodynamic investigation of guide vane configurations downstream a rotating detonation combustor
Experimentelle Untersuchung zum Einfluss des Vorleitrads auf die Rotorströmung eines anderthalbstufigen transsonischen Axialverdichters : = Experimental investigation of the aerodynamic influence of inlet-guide-vanes on the flow features of a one-and-a-half stage axial transonic compressor
Process integration and automated multi-objective optimization supporting aerodynamic compressor design
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The transonic compressor with non-uniform tip clearance: Effects on aerodynamics and aeroelasticity
The transonic compressor with non-uniform tip clearance : effects on aerodynamics and aeroelasticity
An automated multi-objective optimization approach for aerodynamic 3D compressor blade design
"VANeS"
Experimental and Numerical Investigation of a Centrifugal Compressor Stage with Variable Inlet Guide Vanes
Circumferential groove casing treatments in centrifugal compressor aerodynamics
Investigation of the Aerodynamics Characteristics of the Integrated Motor- Compressor
Low-inertia centrifugal compressor wheels: Aerodynamic and mechanical design
Aerodynamic investigation of guide vane configurations downstream a rotating detonation combustor
Experimentelle Untersuchung zum Einfluss des Vorleitrads auf die Rotorströmung eines anderthalbstufigen transsonischen Axialverdichters : = Experimental investigation of the aerodynamic influence of inlet-guide-vanes on the flow features of a one-and-a-half stage axial transonic compressor
Process integration and automated multi-objective optimization supporting aerodynamic compressor design
Diving-flight aerodynamics of a peregrine falcon : = Aerodynamic beim Sturzflug des Wanderfalken
The transonic compressor with non-uniform tip clearance: Effects on aerodynamics and aeroelasticity
The transonic compressor with non-uniform tip clearance : effects on aerodynamics and aeroelasticity
An automated multi-objective optimization approach for aerodynamic 3D compressor blade design
"VANeS"
Experimental and Numerical Investigation of a Centrifugal Compressor Stage with Variable Inlet Guide Vanes
Circumferential groove casing treatments in centrifugal compressor aerodynamics
Investigation of the Aerodynamics Characteristics of the Integrated Motor- Compressor
Low-inertia centrifugal compressor wheels: Aerodynamic and mechanical design
Aerodynamic investigation of guide vane configurations downstream a rotating detonation combustor
Experimentelle Untersuchung zum Einfluss des Vorleitrads auf die Rotorströmung eines anderthalbstufigen transsonischen Axialverdichters : = Experimental investigation of the aerodynamic influence of inlet-guide-vanes on the flow features of a one-and-a-half stage axial transonic compressor
Process integration and automated multi-objective optimization supporting aerodynamic compressor design
Diving-flight aerodynamics of a peregrine falcon : = Aerodynamic beim Sturzflug des Wanderfalken
The transonic compressor with non-uniform tip clearance: Effects on aerodynamics and aeroelasticity
The transonic compressor with non-uniform tip clearance : effects on aerodynamics and aeroelasticity
An automated multi-objective optimization approach for aerodynamic 3D compressor blade design