Tests of a 1/14-scale powered model of the XB-36 airplane in the Langley 19-foot pressure tunnel. : 1 - Stalling characteristics and aileron effectiveness of several wing and flap arrangements /

Tests of a 1/14-scale powered model of the XB-36 airplane in the Langley 19-foot pressure tunnel. : 1 - Stalling characteristics and aileron effectiveness of several wing and flap arrangements / by S.R. Alexander and James C. Sivells.

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An investigation was conducted in the Langley 19-foot pressure tunnel to determine the stalling characteristics, aileron effectiveness, and, to a limited extent, the longitudinal stability of a 1/14-scale model of the XB-36 airplane. The model was tested with the original wing-flap configuration and...

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Bibliographic Details
Main Author: Alexander, S. R.
Corporate Authors: United States. National Advisory Committee for Aeronautics, Langley Aeronautical Laboratory
Other Authors: Sivells, James C.
Other title:NACA Wartime Reports. Series L.
Format: Government Document Book
Language:English
Published: Washington, D.C. : National Advisory Committee for Aeronautics, [1945]
Series:Wartime Reports (United States. National Advisory Committee for Aeronautics) ; no. L624.
Subjects:
Airplanes > Models > Testing.
Ailerons.
Flaps (Airplanes)
Stalling (Aerodynamics)
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/L624
Y 3.N 21/5:11/L624 Available Place a Hold

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