Power-on wind-tunnel tests of the 1/8-scale model of the Brewster F2A airplane with full-span slotted flaps / by John G. Lowry.

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Bibliographic Details
Online Access: Search for the full-text version of this title in HathiTrust
Main Author: Lowry, John G.
Corporate Authors: United States. National Advisory Committee for Aeronautics, Langley Aeronautical Laboratory
Other title:NACA Wartime Reports. Series L.
Technical report archive and image library.
Format: Government Document Book
Language:English
Published: Washington, D.C. : National Advisory Committee for Aeronautics, [1941]
Series:Wartime Reports (United States. National Advisory Committee for Aeronautics) ; no. L707.
Subjects:

MARC

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245 1 0 |a Power-on wind-tunnel tests of the 1/8-scale model of the Brewster F2A airplane with full-span slotted flaps /  |c by John G. Lowry. 
246 3 |a NACA Wartime Reports. Series L. 
260 |a Washington, D.C. :  |b National Advisory Committee for Aeronautics,  |c [1941] 
300 |a 10 pages, 23 unnumbered pages :  |b illustrations ;  |c 27 cm. 
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490 1 |a Wartime Report / National Advisory Committee for Aeronautics ;  |v no. L707. 
500 |a NACA Wartime Report L-707. 
500 |a Originally issued as NACA as Memorandum Report (August 1941) 
500 |a Prepared at the Langley Memorial Aeronautical Laboratory, Langley Field, Virginia. 
504 |a Includes bibliographical references. 
520 3 |a Tests were made in the 7- by 10-foot wind tunnel of the 1/8-scale model of the Brewster F2A airplane with full-span slotted flaps. The object of the tests was to determine the power-one static lateral and longitudinal stability of the complete model with a new wing which had a full-span slotted flap and a plain and slot-lip aileron for lateral control. 
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650 0 |a Airplanes  |x Control. 
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