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

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

Bibliographic Details
Main Author: Suder, Kenneth L.
Corporate Author: United States. National Aeronautics and Space Administration
Format: Government Document Book
Language:English
Published: [Washington, DC] : National Aeronautics and Space Administration ; [1996]
Series:NASA technical memorandum ; 107310.
Subjects:
Flow distribution.
Transonic flow.
Turbocompressors.
Mach number.
Transonic compressors.
Shock wave interaction.

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Call Number: NAS 1.15:107310
 
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NAS 1.15:107310 Available