NDLI: Advances in Engine Test Capabilities at the NASA Glenn Research Center’s Propulsion Systems Laboratory

Content Provider	The American Society of Mechanical Engineers (ASME) Digital Collection
Author	Peter, M. Pachlhofer Joseph, W. Panek Dennis, J. Dicki Barry, R. Piendl Paul, J. Lizanich Gary, A. Klann
Copyright Year	2006
Abstract	The Propulsion Systems Laboratory at the National Aeronautics and Space Administration (NASA) Glenn Research Center is one of the premier U.S. facilities for research on advanced aeropropulsion systems. The facility can simulate a wide range of altitude and Mach number conditions while supplying the aeropropulsion system with all the support services necessary to operate at those conditions. Test data are recorded on a combination of steady-state and high-speed data-acquisition systems. Recently a number of upgrades were made to the facility to meet demanding new requirements for the latest aeropropulsion concepts and to improve operational efficiency. Improvements were made to data-acquisition systems, facility and engine-control systems, test-condition simulation systems, video capture and display capabilities, and personnel training procedures. This paper discusses the facility’s capabilities, recent upgrades, and planned future improvements.
Sponsorship	International Gas Turbine Institute
Starting Page	101
Ending Page	108
Page Count	8
File Format	PDF
ISBN	0791842371
DOI	10.1115/GT2006-90181
e-ISBN	0791837742
Volume Number	Volume 2: Aircraft Engine; Ceramics; Coal, Biomass and Alternative Fuels; Controls, Diagnostics and Instrumentation; Environmental and Regulatory Affairs
Conference Proceedings	ASME Turbo Expo 2006: Power for Land, Sea, and Air
Language	English
Publisher Date	2006-05-08
Publisher Place	Barcelona, Spain
Access Restriction	Subscribed
Subject Keyword	Nasa glenn research center High-mach-number testing Turbine engine testing Propulsion systems laboratory Psl High-altitude testing Jet propulsion Nasa Propulsion systems Engines
Content Type	Text
Resource Type	Article

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