Theoretical performance of an axial-flow compressor in a gas-turbine engine operating with inlet water injection / Reece V. Hensley.

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Bibliographic Details
Main Author:	Hensley, Reece V.
Corporate Author:	United States. National Advisory Committee for Aeronautics
Format:	Government Document Book
Language:	English
Published:	Washington, D.C. : National Advisory Committee for Aeronautics, 1952.
Series:	Technical note (United States. National Advisory Committee for Aeronautics) ; 2673.
Subjects:	Axial flow compressors > Performance. Gas-turbines > Performance.

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Call Number:	Y 3.N 21/5:6/2673
Y 3.N 21/5:6/2673	Available Place a Hold