Freestream Mach-number and temperature measurement in NASA Langley's 20-inch supersonic wind tunnel using laser-induced thermal acoustics /

Bibliographic Details

Main Authors:	Herring, Gregory C. (Author), Balla, R. Jeffrey (Author), Beeler, George B. (Author)
Format:	Government Document eBook
Language:	English
Published:	Hampton, Virginia : National Aeronautics and Space Administration, Langley Research Center, September 2020.
Series:	NASA technical memorandum ; 2020-5007323.
Subjects:	Mach number. Temperature. Freestream measurement. Laser-induced thermal acoustics (LITA) 20-inch supersonic wind tunnel (SWT)
Online Access:	https://purl.fdlp.gov/GPO/gpo146260