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Deutsche Gesellschaft für Luft- und Raumfahrt

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OpenAlex ID: S7407052887
Development of a Digital Twin for Aviation Research
2020 · Meyer, H., Zimdahl, J., et al. · elib (German Aerospace Center) · 28
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Feasibility Analysis and Comparative Assessment of Structural Power Technology in All-Electric Composite Aircraft
2018 · A.E. Scholz, A. Hermanutz, et al. · mediaTUM (Technical University of Munich) · 15
Initial Sizing for a Family of Hybrid-Electric VTOL General Aviation Aircraft
2018 · Finger, D.F., Götten, F., et al. · Deutsche Gesellschaft für Luft- und Raumfahrt · 14
Mass, primary energy, and cost: the impact of optimization objectives on the initial sizing of hybrid-electric general aviation aircraft
2020 · D. Felix Finger, Falk Götten, et al. · CEAS Aeronautical Journal · 13
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MICADO: Overview of Recent Developments within the Conceptual Aircraft Design and Optimization Environment
2021 · Schültke, F., Aigner, B., et al. · RWTH Publications (RWTH Aachen) · 12
Methodology for Design and Evaluation of More Electric Aircraft Systems Architectures within the AVACON Project
2019 · Jünemann, M., Thielecke, F., et al. · tub.dok (Hamburg University of Technology) · 11
Design of a Hybrid Electric Propulsion System within a Preliminary Aircraft Design Software Environment
2018 · B. Aigner, M. Nollmann, et al. · RWTH Publications (RWTH Aachen) · 11
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The Flying V A new Aircraft Configuration for Commercial Passenger Transport
2015 · Benad, J. · Deutsche Gesellschaft für Luft- und Raumfahrt · 11
The New Specific Operations Risk Assessment Approach for UAS Regulation compared to Common Civil Aviation Risk Assessment
2019 · F. Nikodem, J.S. Dittrich, et al. · elib (German Aerospace Center) · 10
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Polaris - Design of Liquid Hydrogen Turbo-Electric Transport Aircraft
2018 · Dietl, T., Karger, J., et al. · Deutsche Gesellschaft für Luft- und Raumfahrt · 10
Parametric Modeling of the Aircraft Electrical Supply System for overall Conceptual Systems Design
2021 · Bielsky, T., Jünemann, M., et al. · tub.dok (Hamburg University of Technology) · 8
Operational Energy and Power Reserves for Hybrid-Electric and Electric Aircraft
2021 · Geiß, I., Strohmayer, A. · Deutsche Gesellschaft für Luft- und Raumfahrt · 6
Systematic Investigation of a Fixed-Pitch Small-Scale Propeller under Non-Axial Inflow Conditions
2021 · Cerny, M., Herzog, N., et al. · mediaTUM – the media and publications repository of the Technical University Munich (Technical University Munich) · 5
Flying with Ice - An Overview of DLR Research in Flight Mechanics with Icing Influence during the Last Decade
2021 · Deiler, C. · elib (German Aerospace Center) · 5
Analysis and Synthesis of Aircraft Configurations during Conceptual Design using an Advanced Morphological Approach
2019 · Bardenhagen, A., Rakov, D. · Deutsche Gesellschaft für Luft- und Raumfahrt · 5
Impact of Electric Taxiing on Hybrid-Electric Aircraft Sizing
2019 · P.C. Vratny, U. Kling · Deutsche Gesellschaft für Luft- und Raumfahrt · 5
Sizing Studies of Light Aircraft with Serial Hybrid Propulsion Systems
2018 · Ludowicy, J., Rings, R., et al. · Deutsche Gesellschaft für Luft- und Raumfahrt · 5
Extensive Investigations on Radial Crack Formation in Labyrinth Seals of Aircraft Engines
2018 · Hühn, L., Rieger, F., et al. · Deutsche Gesellschaft für Luft- und Raumfahrt · 5
Electric Commuter Transport Concept enabled by Combustion Engine Range Extender
2022 · Atanasov, G., van Wensveen, J., et al. · elib (German Aerospace Center) · 4
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Disciplinary Sub-Processes to Assess Low-Speed Performance and Noise Characteristics within an Aircraft Design Environment
2021 · Fröhler, B., Hesse, C., et al. · elib (German Aerospace Center) · 4
Assessment of the Handling Qualities of Multirotor Configurations using Real Time Simulation
2021 · Atci, K., Jones, M., et al. · elib (German Aerospace Center) · 4
A Novel Command Concept for Simplified Vehicle Operations of Onboard Piloted VTOL Transition Aircraft
2021 · Angelov, J., Holzapfel, F. · Deutsche Gesellschaft für Luft- und Raumfahrt · 4
A Map-Based Model for the Determination of Fuel Consumption for Internal Combustion Engines as a Function of Flight Altitude
2020 · Kreyer, J.O., Müller, M., et al. · Deutsche Gesellschaft für Luft- und Raumfahrt · 4
Assessment of a Fuel Cell Powered Full Electric Subsystem Architecture for the Avacon Research Baseline Aircraft
2020 · van Wensveen, J., Peter, F., et al. · Deutsche Gesellschaft für Luft- und Raumfahrt · 4
An Investigation of Electro-Hydraulic High Efficient Power Package Configurations for a More Electric Aircraft System Architecture
2020 · Trochelmann, N., Rave, T., et al. · tub.dok (Hamburg University of Technology) · 4
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Works count: 405
Citation count: 225
H-index: 5
I10-index: 3
2yr mean citedness: 0.118
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