Influence of wall boundary layer upon the performance of an axial-flow fan rotor / Emanuel Boxer.

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Bibliographic Details
Online Access:	Search for the full-text version of this title in HathiTrust
Main Author:	Boxer, Emanuel
Corporate Author:	United States. National Advisory Committee for Aeronautics
Other title:	Technical report archive and image library.
Format:	Government Document Book
Language:	English
Published:	Washington, D.C. : National Advisory Committee for Aeronautics, 1951.
Series:	Technical note (United States. National Advisory Committee for Aeronautics) ; 2291.
Subjects:	Fans (Machinery) Axial flow. Axial flow compressors > Performance. Boundary layer.

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Call Number:	Y 3.N 21/5:6/2291
Y 3.N 21/5:6/2291	Available Place a Hold