Pressure-distribution measurements of a low-drag airfoil with slotted flap submitted by Curtiss-Wright Corporation / by I.H. Abbott.

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Bibliographic Details
Main Author: Abbott, Ira H. A.
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, [1941]
Series:Wartime Reports (United States. National Advisory Committee for Aeronautics) ; no. L676.
Subjects:

MARC

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100 1 |a Abbott, Ira H. A.  |0 http://id.loc.gov/authorities/names/n82040436. 
245 1 0 |a Pressure-distribution measurements of a low-drag airfoil with slotted flap submitted by Curtiss-Wright Corporation /  |c by I.H. Abbott. 
246 3 |a NACA Wartime Reports. Series L. 
260 |a Washington, D.C. :  |b National Advisory Committee for Aeronautics,  |c [1941] 
300 |a 2 pages, 7 unnumbered pages :  |b illustrations ;  |c 27 cm. 
336 |a text  |b txt  |2 rdacontent. 
337 |a unmediated  |b n  |2 rdamedia. 
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490 1 |a Wartime Report / National Advisory Committee for Aeronautics ;  |v no. L676. 
500 |a NACA Wartime Report L-676. 
500 |a Originally issued as NACA as a Memorandum Report (December 1941) 
500 |a Prepared at the Langley Memorial Aeronautical Laboratory, Langley Field, Virginia. 
504 |a Includes bibliographical references. 
520 3 |a Pressure-distribution measurements were made on a 24-inch-chord wooden model equipped with a slotted flap and submitted by the Curtiss-Wright Corporation. The tests were made in the Langley two-dimensional tunnel at a Reynolds number of about 5,600,000. 
520 3 |a The model represented a wing section of the P-60A airplane. The model was equipped with a 0.25c slotted flap with the lip on the upper airfoil surface at approximately 90 percent of the airfoil chord. The model was equipped with pressure-distribution orifices. 
650 0 |a Curtiss-Wright aircraft.  |0 http://id.loc.gov/authorities/subjects/sh85034907. 
650 0 |a Airplanes  |x Models  |x Testing. 
650 0 |a Airplanes  |x Wings.  |0 http://id.loc.gov/authorities/subjects/sh85002923. 
650 0 |a Flaps (Airplanes)  |0 http://id.loc.gov/authorities/subjects/sh85049001. 
650 0 |a Slotted flaps (Airplanes)  |0 http://id.loc.gov/authorities/subjects/sh2007003612. 
650 0 |a Aerodynamic load  |x Measurement. 
650 0 |a Wind tunnel testing.  |0 http://id.loc.gov/authorities/subjects/sh2007008292. 
650 0 |a Charts, diagrams, etc.  |0 http://id.loc.gov/authorities/subjects/sh87002373. 
650 7 |a Aerodynamic load  |x Measurement.  |2 fast  |0 (OCoLC)fst00798184. 
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650 7 |a Charts, diagrams, etc.  |2 fast  |0 (OCoLC)fst00852545. 
650 7 |a Curtiss-Wright aircraft.  |2 fast  |0 (OCoLC)fst00885433. 
650 7 |a Flaps (Airplanes)  |2 fast  |0 (OCoLC)fst00927038. 
650 7 |a Slotted flaps (Airplanes)  |2 fast  |0 (OCoLC)fst01743452. 
650 7 |a Wind tunnel testing.  |2 fast  |0 (OCoLC)fst01744047. 
710 1 |a United States.  |b National Advisory Committee for Aeronautics.  |0 http://id.loc.gov/authorities/names/n79060141  |1 http://isni.org/isni/0000000106642010. 
710 2 |a Langley Aeronautical Laboratory.  |0 http://id.loc.gov/authorities/names/n81018841. 
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