Two-dimensional wind-tunnel investigation of a 10.7-percent-thick symmetrical tail section with a 0.40 airfoil-chord control surface and a 0.20 control-surface-chord tab / Albert L. Braslow.

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Bibliographic Details
Main Author: Braslow, Albert L.
Corporate Author: United States. National Advisory Committee for Aeronautics
Format: Government Document Book
Language:English
Published: Washington D.C. : National Advisory Committee for Aeronautics, 1947.
Series:Technical note (United States. National Advisory Committee for Aeronautics) ; 1228.
Subjects:

MARC

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245 1 0 |a Two-dimensional wind-tunnel investigation of a 10.7-percent-thick symmetrical tail section with a 0.40 airfoil-chord control surface and a 0.20 control-surface-chord tab /  |c Albert L. Braslow. 
260 |a Washington D.C. :  |b National Advisory Committee for Aeronautics,  |c 1947. 
300 |a 14 pages, 24 unnumbered pages :  |b illustrations, tables ;  |c 28 cm. 
336 |a text  |b txt  |2 rdacontent. 
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490 1 |a National Advisory Committee for Aeronautics. Technical Note ;  |v no. 1228. 
500 |a "June 1947." 
500 |a NACA TN number 1228. 
504 |a Includes bibliographical references. 
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650 0 |a Airplanes  |x Control surfaces.  |0 http://id.loc.gov/authorities/subjects/sh85002798. 
650 0 |a Airplanes  |x Tail surfaces.  |0 http://id.loc.gov/authorities/subjects/sh85002903. 
650 0 |a Aerofoils.  |0 http://id.loc.gov/authorities/subjects/sh85001301. 
650 0 |a Flaps (Airplanes)  |0 http://id.loc.gov/authorities/subjects/sh85049001. 
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