The performance of a single-stage impulse turbine having an 11.0-inch pitch-line diameter wheel with cast airfoil-shaped and bent sheet-metal nozzle blades / by David S. Gabriel and L. Robert Carman.

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Bibliographic Details
Online Access:	Search for the full-text version of this title in HathiTrust
Main Author:	Gabriel, David S.
Corporate Authors:	United States. National Advisory Committee for Aeronautics, Aircraft Engine Research Laboratory
Other Authors:	Carman, L. Robert
Other title:	NACA Wartime Reports. Series E. Technical report archive and image library.
Format:	Government Document Book
Language:	English
Published:	Washington, D.C. : National Advisory Committee for Aeronautics, [1945]
Series:	Wartime Reports (United States. National Advisory Committee for Aeronautics) ; no. E233.
Subjects:	Turbines > Compressors > Performance. Waste gases > Combustion gases. Mechanical efficiency. Gas-turbines > Blades. Temperature. Pressure. Charts, diagrams, etc.

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Holdings details from Norlin Library - Basement - Government Information - US
Call Number:	Y 3.N 21/5:11/E233
Y 3.N 21/5:11/E233	Available Place a Hold