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110303s1945 dcua bt f000 0 eng d |
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|a (OCoLC)ocn704935482
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|a (OCoLC)704935482
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|a LHL
|b eng
|c LHL
|d OCLCQ
|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/L32
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|a Y 3.N 21/5:11/L32
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|a NACA WR L32
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|a NACA ARR L5F08b
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|a Heimerl, George J.
|0 http://id.loc.gov/authorities/names/no2007060733.
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|a Column and plate compressive strengths of aircraft structural materials. :
|b Extruded 24S-T aluminum-alloy /
|c by George J. Heimerl and J. Albert Roy.
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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 [1945]
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|a 11 pages, 12 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. L32.
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|a NACA Wartime Report L-32.
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|a Originally issued as NACA as Advance Restricted Report L5F08b (July 1945)
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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 Column and plate compressive strengths of extruded 24S-T aluminum alloy were determined both within and beyond the elastic range from tests of thin-strip columns and local-instability tests of H-, Z-, and channel-section columns. These tests are part of an extensive research investigation to provide data on the structural strength of various aircraft materials. The results are presented in the form of curves and charts that are suitable for use in the design and analysis of aircraft structures.
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|a Airplanes
|x Materials.
|0 http://id.loc.gov/authorities/subjects/sh85002840.
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|a Aluminum alloys.
|0 http://id.loc.gov/authorities/subjects/sh85003975.
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|a Metals
|x Extrusion.
|0 http://id.loc.gov/authorities/subjects/sh85084193.
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|a Columns.
|0 http://id.loc.gov/authorities/subjects/sh85028763.
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|a Strength of materials.
|0 http://id.loc.gov/authorities/subjects/sh85128671.
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|a Charts, diagrams, etc.
|0 http://id.loc.gov/authorities/subjects/sh87002373.
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|a Airplanes
|x Materials.
|2 fast
|0 (OCoLC)fst00803290.
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7 |
|a Aluminum alloys.
|2 fast
|0 (OCoLC)fst00806309.
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|a Charts, diagrams, etc.
|2 fast
|0 (OCoLC)fst00852545.
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7 |
|a Columns.
|2 fast
|0 (OCoLC)fst00868845.
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|a Metals
|x Extrusion.
|2 fast
|0 (OCoLC)fst01018109.
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|a Strength of materials.
|2 fast
|0 (OCoLC)fst01134837.
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|a Roy, J. Albert.
|0 http://id.loc.gov/authorities/names/no2007055106.
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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. L32.
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|a .b95372258
|b 03-19-20
|c 09-22-17
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|a gov
|b 09-22-17
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|i 1
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|a .b95372258
|b 10-02-17
|c 09-22-17
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|a MARS - RDA ENRICHED
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|a .b95372258
|b 09-22-17
|c 09-22-17
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f |
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|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/L32
|h Superintendent of Documents classification
|i document
|m U183073200768
|n 1
|