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02092nam a2200337I 4500 |
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100715e194312 dcua tb f000 0 eng d |
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|a (OCoLC-I)776990891
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|a (OCoLC-M)647971326
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|a LHL
|c LHL
|d LHL
|d CSt
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|a Y 3.N 21/5:6/920
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|a Moore, R. L
|? UNAUTHORIZED
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|a Bearing strengths of bare and alclad XA75S-T and 25S-T81 aluminum alloy sheet /
|c R. L. Moore and C. Wescoat
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|a Washington D.C. :
|b National Advisory Committee for Aeronautics,
|c 1943
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|a 6, [3] p. :
|b ill., tables ;
|c 27 cm
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|a National Advisory Committee for Aeronautics. Technical Note ;
|v no. 920
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|a NACA TN no. 920
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|a "December 1943."
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|a Includes bibliographical references
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|a A report was recently issued covering an investigation of the bearing properties of the wrought aluminum alloys commonly used in aircraft construction. Since this work was undertaken, two new materials, XA75S-T and 24S-T81,have been developed to the commercial stage for aircraft use. THe object of this investigation was to determine the bearing yield and ultimate strengths of these new materials in the form of bare and alclad sheet
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|a Copy 1 bound with 910
|c 9121689 (parent record's ckey)
|b 36105024795077 (item id)
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|a 31
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|a Aluminum alloys
|x Sheet-metal
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|a Loads (Mechanics)
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|a Strength of materials
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|a Wescoat, C
|? UNAUTHORIZED
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|a United States
|b National Advisory Committee for Aeronautics.
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|a Technical note (United States. National Advisory Committee for Aeronautics) ;
|v 920
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|i 48dbfda0-60d1-4bf0-bff1-5319b1087460
|l a9121679
|s US-CST
|m bearing_strengths_of_bare_and_alclad_xa75s_t_and_25s_t81_aluminum_allo_____1943_______natioa________________________________________moore__r__l________________________y_3_n_21_5_6_920p
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|l a9121679
|s ISIL:US-CST
|t BKS
|a SAL3 SEE-OTHER
|b 9121679-1001
|c NACA TN 920
|d ALPHANUM
|x STKS-MONO
|y 9121679-1001
|p UNLOANABLE
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