Development of a gas turbine performance code and its application to preliminary engine design RG Becker, F Wolters, M Nauroz, T Otten | 88 | 2011 |
Collaborative aircraft engine preliminary design using a virtual engine platform, part a: Architecture and methodology S Reitenbach, M Vieweg, R Becker, C Hollmann, F Wolters, J Schmeink, ... AIAA Scitech 2020 Forum, 0867, 2020 | 85 | 2020 |
An integrated method for propulsion system conceptual design RG Becker, S Reitenbach, C Klein, T Otten, M Nauroz, M Siggel Turbo Expo: Power for Land, Sea, and Air 56628, V001T01A021, 2015 | 45 | 2015 |
Optimization of compressor variable geometry settings using multi-fidelity simulation S Reitenbach, M Schnoes, RG Becker, T Otten Turbo Expo: Power for Land, Sea, and Air 56659, V02CT45A010, 2015 | 44 | 2015 |
Collaborative understanding of disciplinary correlations using a low-fidelity physics-based aerospace toolkit E Moerland, RG Becker, B Nagel CEAS Aeronautical Journal 6, 441-454, 2015 | 37 | 2015 |
Urban air mobility research at the DLR German Aerospace Center–Getting the HorizonUAM project started BI Schuchardt, D Becker, RG Becker, A End, T Gerz, F Meller, IC Metz, ... AIAA Aviation 2021 Forum, 3197, 2021 | 36 | 2021 |
Multi-level MDO of a long-range transport aircraft using a distributed analysis framework S Goertz, C Ilic, J Jepsen, M Leitner, M Schulze, A Schuster, J Scherer, ... 18th AIAA/ISSMO multidisciplinary analysis and optimization conference, 4326, 2017 | 34 | 2017 |
Collaborative multi-level MDO process development and application to long-range transport aircraft S Görtz, C Ilic, M Abu-Zurayk, R Liepelt, J Jepsen, T Führer, R Becker, ... ICAS Paper 2016_0345, in Proceedings of the 30th Congress of the …, 2016 | 25 | 2016 |
Sensitivity-based multifidelity multidisciplinary optimization of a powered aircraft subject to a comprehensive set of loads M Abu-Zurayk, A Merle, C Ilic, S Keye, S Goertz, M Schulze, T Klimmek, ... AIAA Aviation 2020 Forum, 3168, 2020 | 23 | 2020 |
Impact of alternative fuels on engine performance and CO2 emissions F Wolters, RG Becker, M Schaefer 28th International Congress of the Aeronautical Sciences (ICAS), Brisbane …, 2012 | 21 | 2012 |
Comparison of a heat soakage model with turbofan transient engine data M Vieweg, F Wolters, RG Becker Turbo Expo: Power for Land, Sea, and Air 50770, V001T01A011, 2017 | 18 | 2017 |
Engine performance simulation of the integrated V2527-Engine Fan F Wolters, R Becker, R Schnell, PB Ebel 54th AIAA Aerospace Sciences Meeting, 0388, 2016 | 16 | 2016 |
Usage of data provenance models in collaborative multi-disciplinary aero-engine design S Reitenbach, M Vieweg, C Hollmann, RG Becker Turbo Expo: Power for Land, Sea, and Air 84096, V02DT38A001, 2020 | 14 | 2020 |
High-fidelity adjoint-based aircraft shape optimization with aeroelastic trimming and engine coupling A Merle, C Ilic, M Abu-Zurayk, J Häßy, RG Becker, M Schulze, T Klimmek EUROGEN Conference, 2019 | 14 | 2019 |
An automated process to create start values for gas turbine performance simulations using neural networks and evolutionary algorithms RG Becker, M Bolemant, D Krause, D Peitsch | 14 | 2015 |
DEPA 2050–Development Pathways for Aviation up to 2050 A Leipold, G Aptsiauri, A Ayazkhani, U Bauder, RG Becker, R Berghof, ... | 12 | 2021 |
Performance analysis of the integrated V2527-engine fan at ground operation R Schnell, PB Ebel, RG Becker, D Schoenweitz | 12 | 2013 |
Preliminary engine design and inlet optimization of the MULDICON concept S Zenkner, M Trost, R Becker, C Voß Aerospace Science and Technology 93, 105318, 2019 | 11 | 2019 |
Performance prediction and progress towards multi-disciplinary design of contra-rotating open rotors S Guérin, R Schnell, RG Becker The Aeronautical Journal 118 (1208), 1159-1179, 2014 | 11 | 2014 |
Can Urban Air Mobility become reality? Opportunities and challenges of UAM as innovative mode of transport and DLR contribution to ongoing research H Pak, L Asmer, P Kokus, BI Schuchardt, A End, F Meller, K Schweiger, ... CEAS Aeronautical Journal, 1-31, 2024 | 10 | 2024 |