Cover Image

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
Description
Item Description:"September 2020."
Physical Description:1 online resource (45 pages, 1 unnumbered page) : color illustrations.