Research Catalog

Experimental investigation of the flow field in a transonic, axial flow compressor, with respect to the development of blockage and loss

Title
Experimental investigation of the flow field in a transonic, axial flow compressor, with respect to the development of blockage and loss / Kenneth L. Suder.
Author
Suder, Kenneth L.
Publication
[Washington, DC] : National Aeronautics and Space Administration ; [Springfield, Va. : National Technical Information Service, distributor, 1996]

Details

Additional Authors
United States. National Aeronautics and Space Administration.
Description
1 v.
Series Statement
NASA technical memorandum ; 107310
Subject
  • Flow distribution
  • Transonic flow
  • Turbocompressors
  • Mach number
  • Transonic compressors
  • Shock wave interaction
Note
  • Shipping list no.: 98-0558-M.
Reproduction (note)
  • Microfiche.
Call Number
READEX Microfiche NAS 1.15:107310
OCLC
marcive42023838
Author
Suder, Kenneth L.
Title
Experimental investigation of the flow field in a transonic, axial flow compressor, with respect to the development of blockage and loss / Kenneth L. Suder.
Imprint
[Washington, DC] : National Aeronautics and Space Administration ; [Springfield, Va. : National Technical Information Service, distributor, 1996]
Series
NASA technical memorandum ; 107310
Reproduction
Microfiche. [Washington, D.C. : National Aeronautics and Space Administration, 1997] 3 microfiches.
Added Author
United States. National Aeronautics and Space Administration.
Gpo Item No.
0830-D (MF)
Sudoc No.
NAS 1.15:107310
Research Call Number
READEX Microfiche NAS 1.15:107310
View in Legacy Catalog