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Richard Becker
Richard Becker
DLR - Institute of Propulsion Technology
在 dlr.de 的电子邮件经过验证 - 首页
标题
引用次数
引用次数
年份
Development of a gas turbine performance code and its application to preliminary engine design
RG Becker, F Wolters, M Nauroz, T Otten
882011
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
852020
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
452015
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
442015
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
372015
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
362021
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
342017
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
252016
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
232020
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
212012
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
182017
Engine performance simulation of the integrated V2527-Engine Fan
F Wolters, R Becker, R Schnell, PB Ebel
54th AIAA Aerospace Sciences Meeting, 0388, 2016
162016
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
142020
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
142019
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
142015
DEPA 2050–Development Pathways for Aviation up to 2050
A Leipold, G Aptsiauri, A Ayazkhani, U Bauder, RG Becker, R Berghof, ...
122021
Performance analysis of the integrated V2527-engine fan at ground operation
R Schnell, PB Ebel, RG Becker, D Schoenweitz
122013
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
112019
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
112014
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
102024
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