Hochschulschrift
Integrated design process for the development of semi-active landing gears for transport aircraft
- Location
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Deutsche Nationalbibliothek Frankfurt am Main
- Dimensions
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21 cm
- Extent
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122 S.
- Language
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Englisch
- Notes
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Ill., graph. Darst.
Stuttgart, Univ., Diss., 2001 (Nicht für den Austausch)
- Keyword
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Flugzeug
Fahrwerk
Stoßdämpfer
Reglerentwurf
- Creator
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Krüger, Wolf
- Table of contents
- Rights
-
Bei diesem Objekt liegt nur das Inhaltsverzeichnis digital vor. Der Zugriff darauf ist unbeschränkt möglich.
- Last update
-
11.06.2025, 2:13 PM 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.
Object type
- Hochschulschrift
Associated
- Krüger, Wolf
Other Objects (12)
Design and analysis of semi-active landing gears for transport aircraft
Advanced conceptual design methods for aircraft landing gears
Integrated design process for the development of semi-active landing gears for transport aircraft
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Hierarchical Optimization of Landing Performance for Lander with Adaptive Landing Gear
Virtual Test Environment for Comprehensive Analysis of Aircraft Landing Gear in Preliminary Design using Co-Simulation
Simulation of landing gear dynamics and brake-gear interaction
Simulation of landing gear dynamics and brake-gear interaction
Control of an electro-hydrostatic actuation system for the nose landing gear of an "all electric aircraft"
Preliminary Weight Estimation for different Actuator Types for Landing Gear Retraction
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Design and analysis of semi-active landing gears for transport aircraft
Advanced conceptual design methods for aircraft landing gears
Integrated design process for the development of semi-active landing gears for transport aircraft
Landing gear positioning and structural mass optimization for a large blended wing body aircraft
Comparison of Electro-Hydraulic and Electro-Mechanic Landing Gear Actuation for Light VTOL Aircraft
Hierarchical Optimization of Landing Performance for Lander with Adaptive Landing Gear
Virtual Test Environment for Comprehensive Analysis of Aircraft Landing Gear in Preliminary Design using Co-Simulation
Simulation of landing gear dynamics and brake-gear interaction
Simulation of landing gear dynamics and brake-gear interaction
Control of an electro-hydrostatic actuation system for the nose landing gear of an "all electric aircraft"
Preliminary Weight Estimation for different Actuator Types for Landing Gear Retraction
Wake vortices of landing aircraft
Design and analysis of semi-active landing gears for transport aircraft
Advanced conceptual design methods for aircraft landing gears
Integrated design process for the development of semi-active landing gears for transport aircraft
Landing gear positioning and structural mass optimization for a large blended wing body aircraft
Comparison of Electro-Hydraulic and Electro-Mechanic Landing Gear Actuation for Light VTOL Aircraft
Hierarchical Optimization of Landing Performance for Lander with Adaptive Landing Gear
Virtual Test Environment for Comprehensive Analysis of Aircraft Landing Gear in Preliminary Design using Co-Simulation
Simulation of landing gear dynamics and brake-gear interaction
Simulation of landing gear dynamics and brake-gear interaction
Control of an electro-hydrostatic actuation system for the nose landing gear of an "all electric aircraft"
Preliminary Weight Estimation for different Actuator Types for Landing Gear Retraction