- Alternative title
-
Vorentwurfsmethoden zur Auslegung von Propulsive Fuselage Flugzeugkonzepten
- Location
-
Deutsche Nationalbibliothek Frankfurt am Main
- Extent
-
Online-Ressource
- Language
-
Englisch
- Notes
-
München, Technische Universität München, Dissertation, 2020
- Keyword
-
Concepts
- Event
-
Veröffentlichung
- (where)
-
München
- (who)
-
Universitätsbibliothek der TU München
- (when)
-
2020
- Creator
-
Bijewitz, Julian Raphael
- Contributor
- URN
-
urn:nbn:de:bvb:91-diss-20201218-1524286-1-9
- Rights
-
Der Zugriff auf das Objekt ist unbeschränkt möglich.
- Last update
-
25.03.2025, 1:45 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
- Bijewitz, Julian Raphael
- Hornung, Mirko
- Friedrichs, Jens
- Universitätsbibliothek der TU München
Time of origin
- 2020
Other Objects (12)
Conceptual Design Methods for Sizing and Performance of Hybrid-Electric Transport Aircraft
Advanced conceptual design methods for aircraft landing gears
Analysis methods for novel cargo aircraft concepts
Advanced methods for propulsion system integration in aircraft conceptual design
Conceptual Design Methods of Electric Power Architectures for Hybrid Energy Aircraft
Consideration of aircraft noise annoyance during conceptual aircraft design
Noise prediction within conceptual aircraft design
Improving aircraft conceptual design with methods for wing loads, aeroelasticity and mass estimation
Influence of flight control laws on structural sizing of commercial aircraft
UNICADO: multidisciplinary analysis in conceptual aircraft design
Conceptual aircraft design for sustainability : nachhaltigkeitsorientierter Flugzeugvorentwurf
Adaptive initial sizing method and safety assessment for hybrid-electric regional aircraft
Conceptual Design Methods for Sizing and Performance of Hybrid-Electric Transport Aircraft
Advanced conceptual design methods for aircraft landing gears
Analysis methods for novel cargo aircraft concepts
Advanced methods for propulsion system integration in aircraft conceptual design
Conceptual Design Methods of Electric Power Architectures for Hybrid Energy Aircraft
Consideration of aircraft noise annoyance during conceptual aircraft design
Noise prediction within conceptual aircraft design
Improving aircraft conceptual design with methods for wing loads, aeroelasticity and mass estimation
Influence of flight control laws on structural sizing of commercial aircraft
UNICADO: multidisciplinary analysis in conceptual aircraft design
Conceptual aircraft design for sustainability : nachhaltigkeitsorientierter Flugzeugvorentwurf
Adaptive initial sizing method and safety assessment for hybrid-electric regional aircraft
Conceptual Design Methods for Sizing and Performance of Hybrid-Electric Transport Aircraft
Advanced conceptual design methods for aircraft landing gears
Analysis methods for novel cargo aircraft concepts
Advanced methods for propulsion system integration in aircraft conceptual design
Conceptual Design Methods of Electric Power Architectures for Hybrid Energy Aircraft
Consideration of aircraft noise annoyance during conceptual aircraft design
Noise prediction within conceptual aircraft design
Improving aircraft conceptual design with methods for wing loads, aeroelasticity and mass estimation
Influence of flight control laws on structural sizing of commercial aircraft
UNICADO: multidisciplinary analysis in conceptual aircraft design
Conceptual aircraft design for sustainability : nachhaltigkeitsorientierter Flugzeugvorentwurf