Demonstration of imaging flow diagnostics using Rayleigh scattering in Langley 0.3-Meter Transonic Cryogenic Tunnel
By: B. Shirinzadeh and G.C. Herring, Toya Barros.
Contributors: Herring, G. C.; Barros, Toya.; Langley Research Center.
Series: NASA/TM -- 1999-208970.; NASA technical memorandum -- 208970.
Publisher: National Aeronautics and Space Administration, Langley Research Center; National Technical Information Service, distributor
Published: 1999
Place of publication: Hampton, Va; [Springfield, Va
Language: eng
Format: Microform
Subjects: Rayleigh scattering; Flow visualization; Charge coupled devices; Nitrogen; Imaging techniques; Transonic wind tunnels; Cryogenics
Notes: Shipping list no.: 99-0703-M.

Microfiche. [Washington, D.C. : National Aeronautics and Space Administration, 1999] 1 microfiche.