J. F. Escuret - Concepedia

Author

J. F. Escuret

MTU Aero Engines (Germany)

Also Known As

J-F Escuret, J. Escuret, J. F. Escuret, J.F. Escuret

Publications

307

Citations

H-Index

Concepts

All Affiliations

MTU Aero Engines (Germany)Rolls-Royce (United Kingdom)

About

J. F. Escuret is an author at MTU Aero Engines (Germany) specializing in aerodynamics, engineering, and space engineering.

Top Concepts

#	Concept	H-Index	Publications	Citations
1	Engineering	5	5	271
2	Space Engineering	5	5	271
3	Computer Engineering	3	3	235
4	Systems Engineering	3	3	231
5	Mechanical Engineering	2	2	36

J. F. Escuret

Publications

295

Citations

H-Index

Page 1

	Year	Citations
Stall Inception and the Prospects for Active Control in Four High-Speed Compressors I. J. Day, Thomas Breuer, J. F. Escuret, Journal of Turbomachinery Four High-speed CompressorsAeroacousticsEarly WarningHigh-speed CompressorsEngineering	1999	113
Stall Inception and the Prospects for Active Control in Four High Speed Compressors I. J. Day, Thomas Breuer, J. F. Escuret, Volume 4: Manufacturing Materials and Metallurgy; Ceramics; Structures and Dynamics; Controls, Diagnostics and Instrumentation; Education; IGTI Scholar Award Early WarningAeroacousticsHigh Speed CompressorsEngineeringAerospace Engineering	1997	93
Stall Inception Measurements in a High-Speed Multistage Compressor J. F. Escuret, Vincent Garnier Journal of Turbomachinery AeroacousticsAerodynamic Flow InstabilitiesUnsteady FlowEngineeringCompressible Flow	1996	29
Tip clearance effect on high-pressure compressor stage matching O. Domercq, J. F. Escuret Proceedings of the Institution of Mechanical Engineers Part A Journal of Power and Energy Loaded HpcEngineeringAerospace EngineeringHigh-pressure CompressorsMechanical Engineering	2007	25
Numerical simulations of surge and rotating-stall in multi-stage axial-flow compressors J. F. Escuret, Vincent Garnier 30th Joint Propulsion Conference and Exhibit Numerical SimulationsCompressible FlowCompressor	1994	24
Effect of a Mismatch Between the Buttons of Variable Stator Vanes and the Flowpath in a Highly Loaded Transonic Compressor Stage J. F. Escuret, Ph. Veysseyre, Michel Villain, Volume 1: Aircraft Engine; Marine; Turbomachinery; Microturbines and Small Turbomachinery AeroacousticsSmooth FlowpathCompressible FlowFlow ControlEngineering	1997	11

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