Sidewall Mach number distributions for the NASA Langley Transonic Dynamics Tunnel
By: James A. Florance and José A. Rivera.
Contributors: Rivera, José A.; Langley Research Center.
Series: NASA/TM -- 2001-211019.; NASA technical memorandum -- 211019.
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.; Calibrating.; Flow measurement.; Pressure measurement.; Turbulent flow.
Notes: Shipping list no.: 2003-0056-M.

Also available via Internet from the NASA web site. Address as of 3/3/03: http://techreports.larc.nasa.gov/ltrs/PDF/2001/tm/NASA-2001-tm211019.pdf ; current access is available via PURL.

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