Results 181 to 190 of about 4,409 (234)

Substantial aircraft contrail formation at low soot emission levels. [PDF]

Nature
Voigt C, Märkl R, Sauer D, Dischl R, Renard C, Seeliger K, Yu F, Kaufmann S, Bräuer T, Jurkat-Witschas T, Le Chenadec G, Moreau J, Requena-Esteban E, Bonne N, Vals M, Roche A, Zelina J, Dörnbrack A, Eirenschmalz L, Heckl C, Horst E, Lichtenstern M, Marsing A, Neumann G, Roiger A, Scheibe M, Stock P, Giez A, Eckel G, Le Clercq P.   +29 more
europepmc   +1 more source

Uncertainty-Aware Remaining Useful Life Prediction via Synergizing TCN-Transformer Networks and Fractional Brownian Motion. [PDF]

Entropy (Basel)
Geng Y, Yu T, Liu Y, Zhao J.
europepmc   +1 more source

Fuel Effects on Aviation Engine Emissions: A Chemical Reactor Network Modeling Study. [PDF]

Energy Fuels
Lopez-Pintor D, MacDonald J, Ramirez-Correa E, Garcia-Oliver JM, Payri R, Marti Gomez-Aldaravi P, Leyland P.   +6 more
europepmc   +1 more source

The Reinforcing Effect of Cluster Materials in the Combustion of Hydrocarbon Fuels. [PDF]

Int J Mol Sci
Wang X, Mu X, Zhang Y, Wang S, Wang R, Wang J.   +5 more
europepmc   +1 more source

Improved sand cat swarm optimization algorithm assisted GraphSAGE-GRU for remaining useful life of engine. [PDF]

Sci Rep
Yuan Y, Li R, Wang G, Lv X.
europepmc   +1 more source

Effects of Intake Distortion on a Turbofan Engine

openaire   +1 more source

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LPV MODELING OF A TURBOFAN ENGINE

IFAC Proceedings Volumes, 2005
Abstract This article describes the application of quasi-LPV modeling techniques to an industrial military turbofan engine simulator developed by Snecma Moteurs, the French aerospace propulsion company. Two approaches are used, classical Jacobian linearization and velocity based linearization. First, we present briefly the theoretical aspects of both
Luc Reberga, Didier Henrion, Jacques Bernussou, Florian Vary   +3 more
openaire   +3 more sources

Thermodynamic Analysis of Turbofan Engine

Volume 1: Turbo Expo 2005, 2005
The present work deals with a detailed parametric thermodynamic analysis of all the possible configurations of turbofan engine (two and three spool with or without mixer and/ afterburner) employing transpiration cooling technique for turbine blade cooling.
R. Yadav, Chandrakant B. Jugseniya, Abhay A. Pashilkar   +2 more
openaire   +2 more sources