Research Catalog

Radial and circumferential flow surveys at the inlet and exit of the Space Shuttle Main Engine High Pressure Fuel Turbine model

Title
Radial and circumferential flow surveys at the inlet and exit of the Space Shuttle Main Engine High Pressure Fuel Turbine model [microform] / S.T. Hudson ... [et al.].
Publication
[Washington, DC : National Aeronautics and Space Administration ; Springfield, Va. : National Technical Information Service, distributor, 1995]

Details

Additional Authors
  • Hudson, S. T.
  • United States. National Aeronautics and Space Administration.
Description
1 v.
Series Statement
NASA TM ; 111116
Uniform Title
NASA technical memorandum ; 111116.
Subject
  • Air flow
  • Aircraft models
  • Flow distribution
  • Flow velocity
  • High pressure
  • Inlet pressure
  • Radial flow
  • Reynolds number
  • Space shuttle main engine
Note
  • Distributed to depository libraries in microfiche.
  • Shipping list no.: 96-0224-M.
Reproduction (note)
  • Microfiche.
Call Number
READEX Microfiche NAS 1.15:111116
OCLC
marcive34615747
Title
Radial and circumferential flow surveys at the inlet and exit of the Space Shuttle Main Engine High Pressure Fuel Turbine model [microform] / S.T. Hudson ... [et al.].
Imprint
[Washington, DC : National Aeronautics and Space Administration ; Springfield, Va. : National Technical Information Service, distributor, 1995]
Series
NASA TM ; 111116
NASA technical memorandum ; 111116.
Reproduction
Microfiche. [Washington, D.C. : National Aeronautics and Space Administration, 1995] 1 microfiche.
Added Author
Hudson, S. T.
United States. National Aeronautics and Space Administration.
Gpo Item No.
0830-D (MF)
Sudoc No.
NAS 1.15:111116
Research Call Number
READEX Microfiche NAS 1.15:111116
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