Climate impact reduction potentials of synthetic kerosene and green hydrogen powered mid-range aircraft concepts

D Silberhorn, K Dahlmann, A Görtz, F Linke, J Zanger… - Applied Sciences, 2022 - mdpi.com
One of aviation's major challenges for the upcoming decades is the reduction in its climate
impact. As synthetic kerosene and green hydrogen are two promising candidates, their …

Collaborative aircraft engine preliminary design using a virtual engine platform, part a: Architecture and methodology

S Reitenbach, M Vieweg, R Becker… - AIAA Scitech 2020 …, 2020 - arc.aiaa.org
As in many other industries, the sector of aircraft engines and gas turbines is also
undergoing a change towards digitalization. The intention is to make digital technologies …

System analysis of turbo-electric and hybrid-electric propulsion systems on a regional aircraft

H Gesell, F Wolters, M Plohr - The Aeronautical Journal, 2019 - cambridge.org
The increasing environmental requirements in the air transport sector pose great challenges
to the aviation industry and are key drivers for innovation. Besides various approaches for …

[PDF][PDF] Assessment of hydrogen fuel tank integration at aircraft level

D Silberhorn, G Atanasov, JN Walther… - Proceedings of the …, 2019 - core.ac.uk
The assessment of different hydrogen tank concepts and shapes at aircraft level for a typical
short/mid-range aircraft with an entry into service of 2045 is the main focus of this paper …

10 years of joint research at DLR and TU Braunschweig toward low-noise aircraft design-what did we achieve?

L Bertsch, W Heinze, S Guérin, M Lummer… - … and Aerospace Open …, 2019 - elib.dlr.de
This review article is based on an invited keynote presentation at the 22ndWorkshop of the
Aero acoustics Specialists Committee of the CEAS. The event was held in September 2018 …

Stability and control investigations in early stages of aircraft design

YJ Hasan, J Flink, S Freund, T Klimmek… - 2018 Applied …, 2018 - arc.aiaa.org
S problems of aircraft are oftentimes detected in later stages of the design phase or even
during flight tests. The associated retroactive design modifications of the aircraft can be very …

Design and application of a multidisciplinary predesign process for novel engine concepts

S Reitenbach, A Krumme… - … for Gas Turbines …, 2019 - asmedigitalcollection.asme.org
The purpose of this paper is to present a multidisciplinary predesign process and its
application to three aero-engine models. First, a twin spool mixed flow turbofan engine …

On the design of a strut-braced wing configuration in a collaborative design environment

E Moerland, T Pfeiffer, D Böhnke, J Jepsen… - 17th AIAA aviation …, 2017 - arc.aiaa.org
I. Introduction he current trend in the industry to upgrade existing aircraft configurations
rather than developing new ones might be an indication for a declining curve of …

System noise assessment of a tube-and-wing aircraft with geared turbofan engines

L Bertsch, F Wolters, W Heinze, M Pott-Pollenske… - Journal of Aircraft, 2019 - arc.aiaa.org
A geared turbofan with an increased bypass ratio promises reduced engine noise
generation if compared to conventional turbofan engines with lower bypass ratios. As a …

An integrated method for propulsion system conceptual design

RG Becker, S Reitenbach… - … Expo: Power for …, 2015 - asmedigitalcollection.asme.org
The conceptual design of future, potentially highly integrated aircraft engines pose a variety
of new design options to the propulsion system engineers. In order to find the best …