Conference Proceeding
Refine
Year of publication
- 2019 (94) (remove)
Institute
- Fachbereich Luft- und Raumfahrttechnik (25)
- Fachbereich Elektrotechnik und Informationstechnik (24)
- Fachbereich Maschinenbau und Mechatronik (13)
- IfB - Institut für Bioengineering (12)
- Fachbereich Medizintechnik und Technomathematik (11)
- Fachbereich Energietechnik (8)
- MASKOR Institut für Mobile Autonome Systeme und Kognitive Robotik (7)
- Fachbereich Bauingenieurwesen (5)
- Fachbereich Wirtschaftswissenschaften (5)
- Solar-Institut Jülich (5)
Document Type
- Conference Proceeding (94) (remove)
Keywords
- Enterprise Architecture (2)
- Aircraft design (1)
- Case Study (1)
- Change Management (1)
- Corporate Culture (1)
- Correlations (1)
- Design rules (1)
- Digital Age (1)
- Digitalisierung (1)
- Diversity Management (1)
- Drag (1)
- Earthquake (1)
- Engineering (1)
- Force (1)
- Geometry (1)
- Geschäftsmodell (1)
- Graph Theory (1)
- Green aircraft (1)
- Hybrid-electric aircraft (1)
- In-plane (1)
- Informationsgesellschaft (1)
- Innovation Management (1)
- Internetökonomie (1)
- Isolation (1)
- Iterative learning control (1)
- Knee (1)
- Load modeling (1)
- Open Data (1)
- Out-of-plane (1)
- Preface (1)
- Resilience Assessment (1)
- Robotic Process Automation (1)
- Seismic (1)
- Software Robots (1)
- Statistics (1)
- Training (1)
- Unmanned Air Vehicle (1)
- Water Supply System (1)
- responsive space (1)
- small solar system body characterisation (1)
- small spacecraft asteroid lander (1)
- small spacecraft solar sail (1)
- system engineering (1)
A review of guidelines and best practices for subsonic aerodynamic simulations using RANS CFD
(2019)
In this paper, an approach to propulsion system modelling for hybrid-electric general aviation aircraft is presented. Because the focus is on general aviation aircraft, only combinations of electric motors and reciprocating combustion engines are explored. Gas turbine hybrids will not be considered. The level of the component's models is appropriate for the conceptual design stage. They are simple and adaptable, so that a wide range of designs with morphologically different propulsive system architectures can be quickly compared. Modelling strategies for both mass and efficiency of each part of the propulsion system (engine, motor, battery and propeller) will be presented.
Application of Low NOx Micro-mix Hydrogen Combustion to 2MW Class Industrial Gas Turbine Combustor
(2019)