Instrumentation development for study of Reynolds analogy in reacting flows
By: D.J. DeTurris.
Contributors: Langley Research Center.
Series: NASA technical memorandum -- 110196.
Publisher: National Aeronautics and Space Administration, Langley Research Center; National Technical Information Service, distributor
Published: 1995
Place of publication: Hampton, Va; [Springfield, Va
Language: eng
Format: Microform
Subjects: Friction measurement.; Heat transfer.; Reacting flow.; Skin friction.; Strain gages.; Supersonic combustion.; Supersonic combustion ramjet engines.; Supersonic flow.; Turbulent boundary layer.; Wall flow.
Notes: Distributed to depository libraries in microfiche.

Shipping list no.: 96-0366-M.

Microfiche. [Washington, D.C. : National Aeronautics and Space Administration, 1995] 1 microfiche.