Public domain
GRC-1994-C-00167
From the collection of NASA Image and Video Library. Free to download, adapt and use — no permission needed.
About this work
A spectrally resolved Rayleigh/Mie scattering diagnostic was developed to measure temperature and wing span wise velocity in the vicinity of an ASTOVL aircraft model tested in the Lewis, now Glenn, 9x15 Low Speed Wind Tunnel. Shown is a Fabry-Perot interferometer that uses only the blue light from a laser to measure static temperature and velocity near the lift nozzles and suction systems.
NASA Image and Video Library’s own descriptionSubjects
Credit lineGRC-1994-C-00167. NASA/GRC, 1994-01-05. Public domain. ID: GRC-1994-C-00167.
