Use of pressure sensitive paint for diagnostics in turbomachinery flows with shocks
By: Jan Lepicovsky, Timothy J. Bencic.
Contributors: Bencic, Timothy J.; NASA Glenn Research Center.
Series: NASA/TM -- 2000-211111.; NASA technical memorandum -- 211111.
Publisher: National Aeronautics and Space Administration, Glenn Research Center; Available from NASA Center for AeroSpace Information
Published: 2000
Place of publication: Cleveland, Ohio; Hanover MD
Language: eng
Format: Microform
Subjects: Pressure sensitive paints.; Turbomachinery.; Internal flow.; Shock waves.
Notes: Shipping list no.: 2002-0367-M.

"November 2001."

Also available via Internet from the NASA web site. Address as of 5/05/03: http://gltrs.grc.nasa.gov/reports/2001/TM-2001-211111.pdf; current access is available via PURL.

Microfiche. [Washington, D.C. : National Aeronautics and Space Administration, 2002?] 1 microfiche.