Results 101 to 110 of about 29,955 (275)

An AD100 implementation of a real-time STOVL aircraft propulsion system [PDF]

open access: yes
A real-time dynamic model of the propulsion system for a Short Take-Off and Vertical Landing (STOVL) aircraft was developed for the AD100 simulation environment.
Drummond, Colin K., Ouzts, Peter J.
core   +1 more source

Preliminary Evaluation of a Turbine/Rotary Combustion Compound Engine for a Subsonic Transport [PDF]

open access: yes
The fuel consumption of a modern compound engine with that of an advanced high pressure ratio turbofan was compared. The compound engine was derived from a turbofan engine by replacing the combustor with a rotary combustion (RC) engine. A number of boost
Civinskas, K. C., Kraft, G. A.
core   +1 more source

Remaining useful life predictions for turbofan engine degradation using semi-supervised deep architecture

open access: yesReliability Engineering & System Safety, 2019
A. L. Ellefsen   +4 more
semanticscholar   +1 more source

Electro-active acoustic liner for the reduction of turbofan noise [PDF]

open access: gold
Édouard Salze   +8 more
openalex   +1 more source

Preliminary study of optimum ductburning turbofan engine cycle design parameters for supersonic cruising [PDF]

open access: yes
The effect of turbofan engine overall pressure ratio, fan pressure ratio, and ductburner temperature rise on the engine weight and cruise fuel consumption for a mach 2.4 supersonic transport was investigated.
Fishbach, L. H.
core   +1 more source

Conditioned pressure spectra and coherence measurements in the core of a turbofan engine [PDF]

open access: yes
Multiple and partial coherence functions and the corresponding conditioned coherent output spectra are computed between fluctuating pressures measured at two locations within the tailpipe of a turbofan engine and far-field acoustic pressure.
Karchmer, A.
core   +1 more source

Outdoor test stand performance of a convertible engine with variable inlet guide vanes for advanced rotorcraft propulsion [PDF]

open access: yes
A variable inlet guide van (VIGV) type convertible engine that could be used to power future high-speed rotorcraft was tested on an outdoor stand. The engine ran stably and smoothly in the turbofan, turboshaft, and dual (combined fan and shaft) power ...
Mcardle, Jack G.
core   +1 more source

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