Turbine engine clearance control systems
Subtitle: current practices and future directions
By: Scott B. Lattime, Bruce M. Steinetz.
Contributors: Steinetz, Bruce M.; NASA Glenn Research Center.
Series: NASA/TM -- 2002-211794.; NASA technical memorandum -- 211794.
Publisher: National Aeronautics and Space Administration, Glenn Research Center; Available from NASA Center for AeroSpace Information
Published: 2002
Place of publication: Cleveland, Ohio; Hanover MD
Language: eng
Format: Microform
Subjects: Blade tip clearance.; Active clearance control.; Engine efficiency.; Turbine seal.; Specific fuel consumption.; Exhaust gas temperature.; High pressure turbine.
Notes: Shipping list no.: 2003-0325-M.

"September 2002."

Also available via Internet from the NASA web site. Address as of 2/12/04: http://gltrs.grc.nasa.gov/reports/2002/TM-2002-211794.pdf; current access available via PURL.

Microfiche. [Washington, D.C. : National Aeronautics and Space Administration, 2003] 1 microfiche.