Hochschulschrift
Preliminary design of propeller-driven aircraft with active high-lift system
- Location
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Deutsche Nationalbibliothek Frankfurt am Main
- ISBN
-
9783947623365
3947623364
- Dimensions
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21 cm, 500 g
- Extent
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xxxvii, 244 Seiten
- Edition
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Als Manuskript gedruckt
- Language
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Englisch
- Notes
-
Illustrationen
Technische Universität Carolo-Wilhelmina zu Braunschweig, Dissertation, 2020
- Bibliographic citation
-
Forschungsbericht / Niedersächsisches Forschungszentrum für Luftfahrt ; 2020, 13
- Classification
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Ingenieurwissenschaften und Maschinenbau
- Event
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Veröffentlichung
- (where)
-
Braunschweig
- (who)
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TU Braunschweig, Niedersächsisches Forschungszentrum für Luftfahrt
- (when)
-
[2020]
- Creator
- Table of contents
- Rights
-
Bei diesem Objekt liegt nur das Inhaltsverzeichnis digital vor. Der Zugriff darauf ist unbeschränkt möglich.
- Last update
-
11.03.2025, 12:36 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.
Object type
- Hochschulschrift
Associated
- Weiss, Tayson William
- Niedersächsisches Forschungszentrum für Luftfahrt
- TU Braunschweig, Niedersächsisches Forschungszentrum für Luftfahrt
Time of origin
- [2020]
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Experiments on propeller influence on a wing with active high lift
Image based measurement techniques for aircraft propeller flow diagnostics : propeller slipstream investigations at high-lift conditions and thrust reverse
Electrically driven, Compact, Transonic Mixed-Flow Compressor for Active High-Lift Systems in Future Aircraft
Design considerations for the electrical power supply of future civil aircraft with active high-lift systems
Supersonic business jets in preliminary aircraft design
Numerical Simulation of the Unsteady Slipstream of Lift Augmenting Distributed Propellers
Automating the Transition of Lift-to-Cruise eVTOL Aircraft
Beaver aircraft parameter identification, technical preparations and preliminary results
Preliminary Design of Integrated Partial Turboelectric Aircraft Propulsion Systems
Preliminary overall aircraft design with hybrid laminar flow control
Preliminary overall aircraft design with hybrid laminar flow control
In-flight lift and drag estimation of an unmanned propeller-driven aircraft
Experiments on propeller influence on a wing with active high lift
Image based measurement techniques for aircraft propeller flow diagnostics : propeller slipstream investigations at high-lift conditions and thrust reverse
Electrically driven, Compact, Transonic Mixed-Flow Compressor for Active High-Lift Systems in Future Aircraft
Design considerations for the electrical power supply of future civil aircraft with active high-lift systems
Supersonic business jets in preliminary aircraft design
Numerical Simulation of the Unsteady Slipstream of Lift Augmenting Distributed Propellers
Automating the Transition of Lift-to-Cruise eVTOL Aircraft
Beaver aircraft parameter identification, technical preparations and preliminary results
Preliminary Design of Integrated Partial Turboelectric Aircraft Propulsion Systems
Preliminary overall aircraft design with hybrid laminar flow control