Highly loaded multi-stage fan drive turbine-tandem blade configuration design / by D.C. Evans and G.W. Wolfmeyer.

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Bibliographic Details
Online Access:	Search for the full-text version of this title in HathiTrust
Main Author:	Evans, D. C.
Corporate Authors:	General Electric Company, Lewis Research Center, United States. National Aeronautics and Space Administration
Other Authors:	Wolfmeyer, G. W.
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], 1972.
Series:	NASA contractor report ; NASA CR-2097.
Subjects:	Airplanes > Turbofan engines > Design and construction. Airplanes > Turbojet engines > Blades > Design and construction.

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Holdings details from Norlin Library - Government Information - US
Call Number:	NAS 1.26:2097
NAS 1.26:2097	Available Place a Hold