Effect of sweep on performance of compressor blade sections as indicated by swept-blade rotor, unswept-blade rotor, and cascade tests / William R. Godwin.

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Bibliographic Details
Main Author:	Godwin, William R.
Corporate Author:	United States. National Advisory Committee for Aeronautics
Format:	Government Document Book
Language:	English
Published:	Washington : National Advisory Committee for Aeronautics, [1957]
Series:	Technical note (United States. National Advisory Committee for Aeronautics) ; 4062.
Subjects:	Axial flow compressors > Blades. Cascades (Fluid dynamics) Compressors > Performance.

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Call Number:	Y 3.N 21/5:6/4062
Y 3.N 21/5:6/4062	Available Place a Hold