D32 Characteristics of New Driving System of Thrust Fan for Turbofan Engine
, 2007 Shunsuke Makino +2 more
openalex +2 more sources
A remote augmentor lift system with a turbine bypass engine [PDF]
Two supersonic vertical takeoff or landing (VTOL) aircraft engine types, a conventional medium bypass ratio turbofan, and a turbine bypass turbojet were studied. The aircraft assumed was a clipped delta wing with canard configuration.
Fishbach, L. H., Franciscus, L. C.
core +1 more source
A Two-Stage Attention-Based Hierarchical Transformer for Turbofan Engine Remaining Useful Life Prediction. [PDF]
Sensors (Basel)Fan Z, Li W, Chang KC.
europepmc +1 more source
Multi-fidelity modelling of a high bypass ratio turbofan engine with variable area nozzle
Andrea Magrini, Ernesto Benini
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Multiple Application Propfan Study (MAPS): Advanced tactical transport [PDF]
This study was conducted to ascertain potential benefits of a propfan propulsion system application to a blended wing/body military tactical transport. Based on a design cruise Mach no.
Liebeck, R. H. +6 more
core +1 more source
Thermodynamics, Environmental and Sustainability Impacts of a Turbofan Engine Under Different Design Conditions Considering Variable Needs in the Aviation Industry. [PDF]
Glob ChallAygun H, Sheikhi MR, Caliskan H.
europepmc +1 more source
Impact Analysis of Intake Air Humidity on Turbofan Engine Performance
, 2018 Shuiming Liu +2 more
openalex +2 more sources
An automated procedure for developing hybrid computer simulations of turbofan engines [PDF]
A systematic, computer-aided, self-documenting methodology for developing hybrid computer simulations of turbofan engines is presented. The methodology makes use of a host program that can run on a large digital computer and a machine-dependent target ...
Krosel, S. M., Szuch, J. R.
core +1 more source
Operating condition and geometry effects on low-frequency afterburner combustion instability in a turbofan at altitude [PDF]
Three afterburner configurations were tested in a low-bypass-ratio turbofan engine to determine the effect of various fuel distributions, inlet conditions, flameholder geometry, and fuel injection location on combustion instability.
Cullom, R. R., Johnsen, R. L.
core +1 more source