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|a (OCoLC)ocn643343681
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|a Y 3.N 21/5:6/412
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|a Anderson, Raymond F.
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|a The Aerodynamic characteristics of airfoils at negative angles of attack /
|c Raymond F. Anderson.
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|a Washington D.C. :
|b National Advisory Committee for Aeronautics,
|c 1932.
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| 300 |
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|a 11 pages, 26 unnumbered pages :
|b illustrations, tables ;
|c 27 cm.
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| 336 |
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|a text
|b txt
|2 rdacontent.
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| 337 |
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|a unmediated
|b n
|2 rdamedia.
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| 338 |
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|a volume
|b nc
|2 rdacarrier.
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|a National Advisory Committee for Aeronautics. Technical Note ;
|v no. 412.
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| 500 |
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|a "March, 1932."
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|a NACA TN number 412.
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|a Includes bibliographical references.
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|a A number of airfoils, including 14 commonly used airfoils and 10 N.A.C.A., were tested through the negative angle-of-attack range in the N.A.C.A. variable density wind tunnel at a Reynolds number of approximately 3,000,000. The tests were made to supply data to serve as a basis for the structural design of airplanes in the inverted flight condition. In order to make the results immediately available for this purpose they are presented herein in preliminary form, together with results of previous tests of airfoils at positive angles of attack.
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|a committed to retain
|c 20230101
|d 20480101
|5 CoU
|f Alliance Shared Trust
|u https://www.coalliance.org/shared-print-archiving-policies.
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|a Aerofoils
|x Wind tunnel testing.
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| 650 |
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|a Angle of attack (Aerodynamics)
|0 http://id.loc.gov/authorities/subjects/sh95010977.
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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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| 830 |
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|a Technical note (United States. National Advisory Committee for Aeronautics) ;
|v 412.
|0 http://id.loc.gov/authorities/names/no2009017392.
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|a .b7933989x
|b 08-13-20
|c 03-23-15
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|a .b7933989x
|b 11-09-19
|c 03-23-15
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|a MARS - RDA ENRICHED
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|a .b7933989x
|b 03-23-15
|c 03-23-15
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|p Can circulate
|a University of Colorado Boulder
|b Boulder Campus
|c Offsite
|d PASCAL Offsite
|e Y 3.N 21/5:6/412
|h Superintendent of Documents classification
|i document
|m P204062603038
|n 1
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