Results 31 to 40 of about 9,897 (232)
DLR TAU-Code uRANS Turbofan Modeling for Aircraft Aerodynamics Investigations
In the context of an increased focus on fuel efficiency and environmental impact, turbofan engine developments continue towards larger bypass ratio engine designs, with Ultra-High Bypass Ratio (UHBR) engines becoming a likely power plant option for ...
Arne Stuermer
doaj +1 more source
Deep-Learning Based Prognosis Approach for Remaining Useful Life Prediction of Turbofan Engine
The entire life cycle of a turbofan engine is a type of asymmetrical process in which each engine part has different characteristics. Extracting and modeling the engine symmetry characteristics is significant in improving remaining useful life (RUL ...
Amgad Muneer +3 more
semanticscholar +1 more source
Analysis of the Application and Benefits of Aircraft Electric Wheel Systems during Taxi and Take-Off
An electric wheel hybrid power system is designed for driving a large single-aisle passenger aircraft during the take-off and ground taxi phases, which consists of an APU, an energy storage system, and a motor.
Shuang Sun +6 more
doaj +1 more source
This research presents a novel methodology for lightweighting and cost reduction of components with high structural demands by integrating advanced design and manufacturing techniques.
Jorge Crespo-Sánchez +4 more
doaj +1 more source
Large and Small Turbofans [PDF]
This article presents a study on common design challenges of large and small turbofans. Turbofan engines powering large transport aircraft have demonstrated much different design objectives than business-jet turbofans including thrust, range, mission type, development cost, unit price, maintainability standards, and production quantities.
openaire +1 more source
On the cavitation-induced collapse erosion of a turbofan fuel pump
Cavitation is a challenging flow phenomenon that can adversely affect the hydraulic performance of centrifugal pumps. In this study, numerical investigations were carried out incorporating the Zwart cavitation model derived from Rayleigh–Plesset equation
Sinopec Wu +3 more
semanticscholar +1 more source
Despite substantial advances in turbofan engineering, a crucial gap persists: there remains the need for an all-inclusive comparative analysis that includes real-world operational data and evaluates the performance of modern turbofans used in aviation ...
Abdulrahman S. Almutairi +3 more
doaj +1 more source
Ammonia for civil aviation: A design and performance study for aircraft and turbofan engine
The 2050 net zero targets for aviation to decarbonize the industry means that solutions need to be delivered that can help achieve those targets. Transitioning to zero carbon aviation fuel is an effective solution to achieve those targets.
Sarath Sasi +5 more
semanticscholar +1 more source
A New Robust Tracking Control Design for Turbofan Engines: H∞/Leitmann Approach
In this paper, a H ∞ /Leitmann approach to the robust tracking control design is presented for an uncertain dynamic system. This new method is developed in the following two steps. Firstly, a tracking dynamic system with simultaneous consideration
Muxuan Pan +3 more
doaj +1 more source
Accurately predicting the remaining useful life (RUL) of the turbofan engine is of great significance for improving the reliability and safety of the engine system.
Amgad Muneer +4 more
semanticscholar +1 more source

