Radial and circumferential flow surveys at the inlet and exit of the Space Shuttle Main Engine High Pressure Fuel Turbine model
By: S.T. Hudson ... [et al.].
Contributors: Hudson, S. T.; United States. National Aeronautics and Space Administration.
Series: NASA TM -- 111116.; NASA technical memorandum -- 111116.
Publisher: National Aeronautics and Space Administration; National Technical Information Service, distributor
Published: 1995
Place of publication: [Washington, DC; Springfield, Va
Language: eng
Format: Microform
Subjects: Air flow.; Aircraft models.; Flow distribution.; Flow velocity.; High pressure.; Inlet pressure.; Radial flow.; Reynolds number.; Space shuttle main engine.
Notes: Distributed to depository libraries in microfiche.

Shipping list no.: 96-0224-M.

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