Pulsed laser Rayleigh scattering diagnostic for hyrogen/oxygen rocket exit plane flowfield velocimetry
By: Frank J. Zupanc.
Contributors: United States. National Aeronautics and Space Administration.
Series: NASA technical memorandum -- 106213
Publisher: National Aeronautics and Space Administration; National Technical Information Service, distributor
Published: 1993
Place of publication: [Washington, DC]; [Springfield, Va
Language: eng
Format: Microform
Subjects: Rayleigh scattering.; Rocket engines -- Thrust.; Fluid dynamic measurements.
Notes: Distributed to depository libraries in microfiche.

Shipping list no.: 93-1215-M.

Microfiche. [Washington, D.C. : National Aeronautics and Space Administration, 1993] 1 microfiche.