Langley 16-ft. Transonic Tunnel Pressure Sensitive Paint System
By: Danny R. Sprinkle ... [et al.].
Contributors: Sprinkle, Danny R.; Langley Research Center.
Series: NASA/TM -- 2001-211017; NASA technical memorandum -- 211017.
Publisher: National Aeronautics and Space Administration, Langley Research Center; Available from NASA Center for AeroSpace Information (CASI)
Published: 2001
Place of publication: Hampton, Va; Hanover MD
Language: eng
Format: Microform
Subjects: Transonic wind tunnels.; Pressure sensitive paints.; Pressure measurement.; Flow visualization.
Other titles: Langley Sixteen Foot Transonic Tunnel Pressure Sensitive Paint System
Notes: Shipping list no.: 2003-0056-M.

Also available via Internet from the NASA web site. Address as of 3/19/03: http://techreports.larc.nasa.gov/ltrs/PDF/2001/tm/NASA-2001-tm211017.pdf; current access is available via PURL.

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