Effect of afterburner lights and inlet unstarts on a mixed compression inlet turbofan engine operating at Mach 2.5 [PDF]
Data are presented to show the response of an uncontrolled inlet to afterburner lightoff disturbances when a mixed-compression inlet is coupled to a turbofan engine.
Batterton, P. G. +2 more
core +1 more source
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
Dynamic Analysis and Experimental Research on the Cantilever High Speed Rotor of Turbofan Engine
Weijian Nie +3 more
openalex +1 more source
Utilizing numerical techniques in turbofan inlet acoustic suppressor design [PDF]
Numerical theories in conjunction with previously published analytical results are used to augment current analytical theories in the acoustic design of a turbofan inlet nacelle. In particular, a finite element-integral theory is used to study the effect
Baumeister, K. J.
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Summary of recent investigations of inlet flow distortion effect on engine stability [PDF]
A review is presented of recent experimental results, analytical procedures and test techniques employed to evaluate the effects of inlet flow distortion on the stability characteristics of representative afterburning turbofan and turbojet compression ...
Braithwaite, W. M., Graber, E. J., Jr.
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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
Adaptive Degradation Prognostic Reasoning by Particle Filter with a Neural Network Degradation Model for Turbofan Jet Engine [PDF]
Faisal Khan +3 more
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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
Failure Mode and Effects Analysis on the Air System of an Aero Turbofan Engine Using the Gaussian Model and Evidence Theory. [PDF]
Tang Y, Zhou Y, Zhou Y, Huang Y, Zhou D.
europepmc +1 more source
Time Delay Analysis of Turbofan Engine Direct and Indirect Combustion Noise Sources [PDF]
Jeffrey Hilton Miles
openalex +1 more source

