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02056nam a2200301I 4500 |
| 001 |
65097e87-0358-4791-a6be-7494ba33b766 |
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20230617000000.0 |
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100713e194212 dcua t f000 0 eng d |
| 035 |
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|a (OCoLC-I)776888798
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|a (OCoLC-M)647415468
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|a LHL
|c LHL
|d UtOrBLW
|d CSt
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|a Y 3.N 21/5:6/877
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| 100 |
1 |
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|a Paul, D. A
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|a An Exploration of the longitudinal tensile and compressive properties throughout an extruded shape of 24S-T aluminum alloy /
|c D. A. Paul
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|a Washington D.C. :
|b National Advisory Committee for Aeronautics,
|c 1942
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| 300 |
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|a 9, [3] p. :
|b ill., tables ;
|c 27 cm
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| 490 |
1 |
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|a National Advisory Committee for Aeronautics. Technical Note ;
|v no. 877
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| 500 |
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|a NACA TN no. 877
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|a "December 1942."
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|a Tensile and compressive properties were investigated of specimens cut from the extruded shape of 24S-T aluminum alloy. The tensile strengths, tensile yield strengths, elongations, and compressive yield strengths of both the unrecrystallized and the recrystallized portions were determined. The strength of a cross section of an extruded shape is the weighted average of the strengths of the unrecrystallized and the recrystallized areas. The strength of an extruded shape varies along the length of the extrusion
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|a Copy 1 bound with 869
|c 9121730 (parent record's ckey)
|b 36105024795119 (item id)
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| 596 |
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|a 31
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| 650 |
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|a Aluminum alloys
|x Testing
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| 650 |
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0 |
|a Strength of materials
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| 710 |
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|a United States
|b National Advisory Committee for Aeronautics.
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| 830 |
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|a Technical note (United States. National Advisory Committee for Aeronautics) ;
|v 877
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| 999 |
1 |
0 |
|i 65097e87-0358-4791-a6be-7494ba33b766
|l a9121721
|s US-CST
|m exploration_of_the_longitudinal_tensile_and_compressive_properties_thr_____1942_______natioa________________________________________paul__d__a_________________________y_3_n_21_5_6_877p
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| 999 |
1 |
1 |
|l a9121721
|s ISIL:US-CST
|t BKS
|a SAL3 SEE-OTHER
|b 9121721-1001
|c NACA TN 877
|d ALPHANUM
|x STKS-MONO
|y 9121721-1001
|p UNLOANABLE
|