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‡a(MiU)99187539586606381
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‡asdr-miu.99187539586606381
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‡aD 301.45/26-2:61-692
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‡aAD 290770
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‡aASD TR 61-692
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‡aCrawford, Robert F.,
‡eauthor.
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‡aStrength, efficiency, and design data for beryllium structures /
‡cRobert F. Crawford, A. Bruce Burns.
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‡aWright-Patterson Air Force Base, Ohio :
‡bFlight Dynamics Laboratory, Aeronautical Systems Command, Air Force Systems Command, United States Air Force,
‡c1962.
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‡axxxiv, [484] pages :
‡billustrations, tables ;
‡c28 cm.
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‡atext
‡btxt
‡2rdacontent
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‡aunmediated
‡bn
‡2rdamedia
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‡avolume
‡bnc
‡2rdacarrier
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‡aAeronautical Systems Division (U.S.). Technical Report ;
‡vASD TR 61-692
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‡aAD0290770 (from http://www.dtic.mil).
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‡a"February 1962."
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‡aIncludes bibliographical references.
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‡aStudies were made to investigate the design capabilities of beryllium as a structural material and to derive and develop structural design curves and related data for efficient structural design with beryllium. The metal beryllium is believed to have high potential for aerospace structures, but is not extensively considered in design applications because of uncertainties as to the proper design procedures. This report presents information based on studies and tests which clearly shows that beryllium now may be designed with confidence into many types of load-carrying structures, using well-known methods of structural analysis and appropriate margins of safety. The resulting beryllium structures are shown to be considerably lighter than identical structures fabricated from other metals, and these structures are attainable with currently available beryllium mill products.
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‡aResearch supported by the United States Air Force, Air Force Systems Command, and performed by Lockheed Missiles and Space Company, Sunnyvale, California, under Contract No.
‡bAF 33(616)-6905.
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‡aMode of access: Internet.
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7 |
‡aStructural engineering.
‡2fast
‡0(OCoLC)fst01135658
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‡aBeryllium.
‡2fast
‡0(OCoLC)fst00830825
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‡aStructural engineering.
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‡aBeryllium.
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‡aBurns, A. Bruce,
‡eauthor.
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‡aUnited States.
‡bAir Force.
‡bSystems Command.
‡bAeronautical Systems Division,
‡eissuing body.
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‡aLockheed Missiles and Space Company,
‡esponsor.
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‡aTechnical Report Archive & Image Library (TRAIL)
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