Performance of a 1.15-pressure-ratio axial-flow fan stage with a blade tip solidity of 0.5 / by Walter M. Osborn and Ronald J. Steinke.

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Bibliographic Details
Online Access:	Search for the full-text version of this title in HathiTrust
Main Author:	Osborn, Walter Martin, 1918-
Corporate Authors:	Lewis Research Center, United States. National Aeronautics and Space Administration
Other Authors:	Steinke, Ronald J.
Format:	Government Document Book
Language:	English
Published:	Washington, D.C. : [Springfield, Va.] : National Aeronautics and Space Administration ; [For sale by the National Technical Information Service], 1974.
Series:	NASA technical memorandum ; X-3052.
Subjects:	Axial flow compressors > Testing > Statistics. Airplanes > Turbofan engines.

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Holdings details from Norlin Library - Government Information - US
Call Number:	NAS 1.15:3052
NAS 1.15:3052	Available Place a Hold