WInd-tunnel tests of ailerons at various speeds. : 4 - Ailerons of 0.20 airfoil chord and true contour with 0.35 aileron-chord extreme blunt-nose balance on the NACA 23012 airfoil /

WInd-tunnel tests of ailerons at various speeds. : 4 - Ailerons of 0.20 airfoil chord and true contour with 0.35 aileron-chord extreme blunt-nose balance on the NACA 23012 airfoil / by W. Letko, T.A. Hollingworth, and R.A. Anderson.

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Tests were made on an NACA 23012 airfoil fitted with a 20-percent-chord, true-contour aileron with 35-percent-chord, extreme blunt-nose balance. The tests were made in the two-dimensional test section of the NACA stability tunnel at a range of airspeeds from 160 to 360 miles per hour, which correspo...

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Bibliographic Details
Main Author: Letko, W.
Corporate Authors: United States. National Advisory Committee for Aeronautics, Langley Aeronautical Laboratory
Other Authors: Hollingworth, Thomas A., Anderson, R. A.
Other title:NACA Wartime Reports. Series L.
Format: Government Document Book
Language:English
Published: Washington, D.C. : National Advisory Committee for Aeronautics, [1943]
Series:Wartime Reports (United States. National Advisory Committee for Aeronautics) ; no. L433.
Subjects:
Ailerons.
Aerofoils.
Air speed.
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/L433
Y 3.N 21/5:11/L433 Available Place a Hold

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