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décrochage du compresseur

compressor stall

industrie mécanique - iate.europa.eu

Ensuite, il démontre une capacité à descendre la queue la première sans provoquer un décrochage du compresseur.

Then it demonstrates an ability to descend tail first without causing a compressor stall.

général - CCMatrix (Wikipedia + CommonCrawl)

L’accident a été attribué à un décrochage du compresseur, a rapporté l’armée de l’air en juin à la suite d’une enquête.

That crash was blamed on a compressor stall, the Air Force reported in June following an investigation.

général - CCMatrix (Wikipedia + CommonCrawl)

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Design optimisation of circumferential casing groove for stall margin improvement in a transonic compressor rotor... A Random Forest surrogate model is coupled with a Multi-Objective Genetic Algorithm optimiser to determine the optimum casing groove sizing and location that improves the compressor stall margin....

industrie mécanique - core.ac.uk - PDF: 3af-aerodynamics2019.com

Experimental investigation of high-pressure steam-induced surge in a transonic compressor stage... The primary goals of this research were to quantify changes in the compressor stall margin as a result of steam ingestion and to develop pressure contour maps to analyze the transformation of shock structures in the blade passages as they relate...

PDF: calhoun.nps.edu

décrochage du compresseur

engine stall

industrie mécanique - iate.europa.eu

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Predicted performance benefits of an adaptive digital engine control system of an f-15 airplane... The ADECS mode is a highly integrated mode in which the airplane flight conditions, the resulting inlet distortion, and the available engine stall margin are continually computed....

général - core.ac.uk - PDF: hdl.handle.net

A simulator evaluation of pilot response to an aircraft cockpit spin indicator system.... The time required to correctly respond to departedflight, spin, and engine stall indications was measured usingF-14 NATOPS procedures....

PDF: archive.org

Investigation of avionic events with use of information from on-board recorders of flight parameters... Subsequently the effect of the engine stall is outlined, which enables analysis of those avionic events when the effect of engine(s) stall took place....

PDF: yadda.icm.edu.pl

Highly integrated digital engine control system on an f-15 airplane... An integrated flightpath management mode and an integrated adaptive engine stall margin mode are implemented into the system....

PDF: hdl.handle.net

Test and evaluation of the hidec engine uptrim algorithm... Performance improvements will result from an adaptive engine stall margin mode, a highly integrated mode that uses the airplane flight conditions and the resulting inlet distortion to continuously compute engine stall margin....

PDF: hdl.handle.net

Publications scientifiques

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Investigation at supersonic speeds of the compressor stall and inlet buzz characteristics of a j34 - spike-inlet combination /... Approaching the inlet buzz limit with the engine operating in or near a stall condition did not affect the minimum stable air flow of the diffuser, and conversely the presence of mild buzz did not affect the compressor stall limit....

général - core.ac.uk - PDF: www.hathitrust.org

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Nonlinear global stability analysis of compressor stall phenomenaCompressor stall phenomena are analyzed from the point of view of nonlinear control theory, based on bifurcation-catastrophe techniques....

général - core.ac.uk - PDF: hdl.handle.net

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Inlet unstart propulsion integration wind tunnel test program completed for high-speed civil transport... Adverse transient phenomena such as engine compressor stall and inlet unstart could severely degrade the performance of one of these propulsion pods....

général - core.ac.uk - PDF: hdl.handle.net