Hochschulschrift
Landing gear positioning and structural mass optimization for a large blended wing body aircraft
- Location
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Deutsche Nationalbibliothek Frankfurt am Main
- Dimensions
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21 cm
- Extent
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xiii, 139 Seiten
- Language
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Englisch
- Notes
-
Illustrationen
Technische Universität München, Dissertation, 2013
- Bibliographic citation
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Forschungsbericht ; 2014,20
- Event
-
Veröffentlichung
- (where)
-
Köln
- (who)
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DLR, Deutsches Zentrum für Luft- und Raumfahrt
- (when)
-
[2014]
- Creator
- Table of contents
- Rights
-
Bei diesem Objekt liegt nur das Inhaltsverzeichnis digital vor. Der Zugriff darauf ist unbeschränkt möglich.
- Last update
-
11.06.2025, 2:05 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
- Cumnuantip, Sunpeth
- DLR, Deutsches Zentrum für Luft- und Raumfahrt
Time of origin
- [2014]
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Die Blended Wing Body (BWB) Flugzeugkonfiguration : The blended wing body (BWB) aircraft configuration
Advanced conceptual design methods for aircraft landing gears
The virtual landing pad: facilitating rotary-wing landing operations in degraded visual environments
Main Landing Gear Operation powered by Multifunctional High-Lift PCUs
Landing Gear Design and Assessment Methodology in the AVACON Project
The landing gear system in multi-machine Hybrid Event-B
Design and analysis of semi-active landing gears for transport aircraft
Preliminary Weight Estimation for different Actuator Types for Landing Gear Retraction
Simulation of landing gear dynamics and brake-gear interaction
Simulation of landing gear dynamics and brake-gear interaction
Hierarchical Optimization of Landing Performance for Lander with Adaptive Landing Gear
The blended wing body (BWB) aircraft configuration : Die Blended Wing Body (BWB) Flugzeugkonfiguration
Die Blended Wing Body (BWB) Flugzeugkonfiguration : The blended wing body (BWB) aircraft configuration
Advanced conceptual design methods for aircraft landing gears
The virtual landing pad: facilitating rotary-wing landing operations in degraded visual environments
Main Landing Gear Operation powered by Multifunctional High-Lift PCUs
Landing Gear Design and Assessment Methodology in the AVACON Project
The landing gear system in multi-machine Hybrid Event-B
Design and analysis of semi-active landing gears for transport aircraft