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110331s1941 dcua bt f000 0 eng d |
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|a (OCoLC)ocn710061403
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|a (OCoLC)710061403
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|a LHL
|b eng
|c LHL
|d LHL
|d OCLCF
|d OCLCO
|d OCLCQ
|d COD
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|a COD9
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|a Y 3.N 21/5:11/L676
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|a Y 3.N 21/5:11/L676
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|a NACA WR L676
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|a Abbott, Ira H. A.
|0 http://id.loc.gov/authorities/names/n82040436.
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|a Pressure-distribution measurements of a low-drag airfoil with slotted flap submitted by Curtiss-Wright Corporation /
|c by I.H. Abbott.
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|a NACA Wartime Reports. Series L.
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|a Washington, D.C. :
|b National Advisory Committee for Aeronautics,
|c [1941]
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|a 2 pages, 7 unnumbered pages :
|b illustrations ;
|c 27 cm.
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|a text
|b txt
|2 rdacontent.
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|a unmediated
|b n
|2 rdamedia.
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|a volume
|b nc
|2 rdacarrier.
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|a Wartime Report / National Advisory Committee for Aeronautics ;
|v no. L676.
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|a NACA Wartime Report L-676.
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|a Originally issued as NACA as a Memorandum Report (December 1941)
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|a Prepared at the Langley Memorial Aeronautical Laboratory, Langley Field, Virginia.
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|a Includes bibliographical references.
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|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.
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|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.
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|a Curtiss-Wright aircraft.
|0 http://id.loc.gov/authorities/subjects/sh85034907.
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|a Airplanes
|x Models
|x Testing.
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|a Airplanes
|x Wings.
|0 http://id.loc.gov/authorities/subjects/sh85002923.
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|a Flaps (Airplanes)
|0 http://id.loc.gov/authorities/subjects/sh85049001.
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|a Slotted flaps (Airplanes)
|0 http://id.loc.gov/authorities/subjects/sh2007003612.
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|a Aerodynamic load
|x Measurement.
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|a Wind tunnel testing.
|0 http://id.loc.gov/authorities/subjects/sh2007008292.
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|a Charts, diagrams, etc.
|0 http://id.loc.gov/authorities/subjects/sh87002373.
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|a Aerodynamic load
|x Measurement.
|2 fast
|0 (OCoLC)fst00798184.
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|a Airplanes
|x Models
|x Testing.
|2 fast
|0 (OCoLC)fst00803318.
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|a Airplanes
|x Wings.
|2 fast
|0 (OCoLC)fst00803545.
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|a Charts, diagrams, etc.
|2 fast
|0 (OCoLC)fst00852545.
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|a Curtiss-Wright aircraft.
|2 fast
|0 (OCoLC)fst00885433.
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|a Flaps (Airplanes)
|2 fast
|0 (OCoLC)fst00927038.
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|a Slotted flaps (Airplanes)
|2 fast
|0 (OCoLC)fst01743452.
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|a Wind tunnel testing.
|2 fast
|0 (OCoLC)fst01744047.
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|a United States.
|b National Advisory Committee for Aeronautics.
|0 http://id.loc.gov/authorities/names/n79060141
|1 http://isni.org/isni/0000000106642010.
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|a Langley Aeronautical Laboratory.
|0 http://id.loc.gov/authorities/names/n81018841.
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|a Wartime Reports (United States. National Advisory Committee for Aeronautics) ;
|v no. L676.
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|a .b97764723
|b 03-19-20
|c 11-06-17
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|a gov
|b 11-06-17
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|f eng
|g dcu
|h 0
|i 1
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|a .b97764723
|b 12-19-17
|c 11-06-17
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|a MARS - RDA ENRICHED
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|a .b97764723
|b 11-06-17
|c 11-06-17
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|a gro17/18:cjg
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|i 228709a6-9058-5bb6-bb12-87f73eb2110f
|s e57ec60b-cf1d-5764-851e-03beb2ad72c8
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f |
f |
|p Can circulate
|a University of Colorado Boulder
|b Boulder Campus
|c Norlin
|d Norlin Library - Basement - Government Information - US
|e Y 3.N 21/5:11/L676
|h Superintendent of Documents classification
|i document
|m U183073228669
|n 1
|