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Silberhorn, Daniel
in Cooperation with on an Cooperation-Score of 37%
Topics
Publications (13/13 displayed)
- 2023Operating narrow-body aircraft with power-to-liquid and liquid hydrogen propulsion: An economic analysis under uncertainty
- 2022Refueling of LH2 Aircraft—Assessment of Turnaround Procedures and Aircraft Design Implicationcitations
- 2022Refueling of LH2 Aircraft—Assessment of Turnaround Procedures and Aircraft Design Implicationcitations
- 2022A Detailed and Comparative Economic Analysis of Hybrid-Electric Aircraft Concepts Considering Environmental Assessment Factorscitations
- 2022Analytical fuselage structure mass estimation using the PANDORA framework
- 2022Climate Impact Reduction Potentials of Synthetic Kerosene and Green Hydrogen Powered Mid-Range Aircraft Conceptscitations
- 2022Impact of the Number of Wing Stations on the Twist Distribution of a BWB Conceptual Aircraft Design in a MDAO Environment to Match Target Lift Distribution
- 2021Overview of the DLR activities in Clean Sky 2 regarding novel configurations and hybrid electric aircraft
- 2021Short Medium Range Turboprop-Powered Aircraft as an Enabler for Low Climate Impact
- 2020Preliminary Aircraft Design within a Multidisciplinary and Multifidelity Design Environment
- 2020Conceptual Design Studies of Boosted Turbofan Configuration for short rangecitations
- 2020Application of a turbo electric aircraft design environment for boosted turbofan aircraft configuration studies
- 2019Minimalistic Use of Hybrid-Electric Technologies for Aircraft Performance Improvement in Off-Design Operation
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conferencepaper
Overview of the DLR activities in Clean Sky 2 regarding novel configurations and hybrid electric aircraft
Abstract
The activities at the German Aerospace Center (DLR) during the last years in Clean Sky 2 within the Large Passenger Aircraft (LPA) and in the scope of AdvanceD Engine and Aircraft Configurations (ADEC) are presented. Here, the evaluation process, the DLR's Remote Control Environment (RCE) overall aircraft design (OAD) workflow and the results of the corresponding conceptual design studies of unconvetional configurations and hybrid electric aircraft are shown.
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