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20240926000000.0 |
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100712e194109 dcua tb f000 0 eng d |
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|a (OCoLC-I)776704555
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|a (OCoLC-M)646826610
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|a (Sirsi) o646826610
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|a (Sirsi) ocn646826610
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|a LHL
|c LHL
|d OCLCQ
|d CSt
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|a Y 3.N 21/5:6/826
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|a Howell, F. M
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|a Variation of properties throughout cross section of two extruded shapes /
|c F. M. Howell
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|a Washington D.C. :
|b National Advisory Committee for Aeronautics,
|c 1941
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|a 6, [7] p. :
|b ill., tables ;
|c 27 cm
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|a National Advisory Committee for Aeronautics. Technical Note ;
|v no. 826
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|a NACA TN no. 826
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|a "September 1941."
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|a Includes bibliographical references
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|a Tensile and and compressive properties were determined of specimens cut from the fins and the main bodies of two different extruded shaps of 24S-T aluminum alloy. The specimens from the fins as compared with those from the main body of the section showed: tensile strengths from 5,000 to 10,000 pounds per square inch lower; tensile yield strengths and compressive yield strengths 4000 to 9000 pounds per square inch lower. The compressive yield strength values for any given location in the cross sections were about 1000 to 6000 pounds per square inch inch lower than the tensile yield strength values for the same location
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|a Copy 1 bound with 824
|c 9121637 (parent record's ckey)
|b 36105024794922 (item id)
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|a Aluminum alloys
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|a Materials
|x Compression testing
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|a Metals
|x Extrusion
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|a Strength of materials
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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 826
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1 |
0 |
|i 6bf1bbdc-d2ee-47f2-b25a-b2b48ffe8dfe
|l a9121611
|s US-CST
|m variation_of_properties_throughout_cross_section_of_two_extruded_shape_____1941_______natioa________________________________________howell__f__m_______________________y_3_n_21_5_6_826p
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999 |
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|l a9121611
|s ISIL:US-CST
|t BKS
|b c902f435-22a3-5ff0-8ec9-1459027fa43b
|y c902f435-22a3-5ff0-8ec9-1459027fa43b
|p UNLOANABLE
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999 |
1 |
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|l a9121611
|s ISIL:US-CST
|t BKS
|a SAL3-SEE-OTHER
|c NACA TN 826
|d Shelving control number
|p UNLOANABLE
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