Effect of Mach number on position error as applied to a pitot-static tube located 0.55 chord ahead of an airplane wing / by W.F. Lindsey.

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Bibliographic Details
Main Author:	Lindsey, W. F.
Corporate Authors:	United States. National Advisory Committee for Aeronautics, Langley Aeronautical Laboratory
Other title:	NACA Wartime Reports. Series L.
Format:	Government Document Book
Language:	English
Published:	Washington, D.C. : National Advisory Committee for Aeronautics, [1944]
Series:	Wartime Reports (United States. National Advisory Committee for Aeronautics) ; no. L75.
Subjects:	Aerofoils. Compressibility. Pitot tubes. Mach number. Wind tunnel testing. Charts, diagrams, etc.

Norlin Library - Basement - Government Information - US

Holdings details from Norlin Library - Basement - Government Information - US
Call Number:	Y 3.N 21/5:11/L75
Y 3.N 21/5:11/L75	Available Place a Hold