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.