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03513nam a2200601Ii 4500 |
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9a4c530c-72d2-4e08-a973-4117f4f9cef0 |
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20240811000000.0 |
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190508s1954 dcua ob f000 0 eng d |
035 |
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|a (OCoLC)1100474456
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|a (OCoLC-M)1195706414
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|a TRAAL
|b eng
|e rda
|e pn
|c TRAAL
|d OCLCO
|d COP
|d TRAAL
|d GPO
|d MvI
|d UtOrBLW
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040 |
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|a TRAAL
|b eng
|e rda
|e pn
|c TRAAL
|d OCLCO
|d COP
|d TRAAL
|d GPO
|d MvI
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|a 9999 (online)
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0 |
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|a Y 3.N 21/5:6/3269
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100 |
1 |
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|a Hartmann, E. C.,
|e author
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245 |
1 |
0 |
|a Additional static and fatigue tests of high-strength aluminum-alloy bolted joints /
|c by E.C. Hartmann, Marshall Holt, and I.D. Eaton
|
264 |
|
1 |
|a Washington, [D.C.] :
|b National Advisory Committee for Aeronautics,
|c 1954
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300 |
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|a 1 online resource (42 pages) :
|b illustrations
|
336 |
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|a text
|b txt
|2 rdacontent
|
337 |
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|a computer
|b c
|2 rdamedia
|
338 |
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|a online resource
|b cr
|2 rdacarrier
|
490 |
1 |
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|a Technical notes / National Advisory Committee for Aeronautics ;
|v No. 3269
|
500 |
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|a No Federal Depository Library Program (FDLP) item number
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500 |
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|a "July 1954."
|
504 |
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|a Includes bibliographical references (page 14)
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588 |
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|a Description based on online resource, PDF version; title from title page (TRAIL, viewed August 7, 2020)
|
596 |
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|a 22
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650 |
|
0 |
|a Aluminum alloys
|x Fatigue
|= ^A991809
|
650 |
|
0 |
|a Aluminum alloys
|x Fatigue
|
650 |
|
0 |
|a Bolted joints
|x Testing
|
650 |
|
0 |
|a Joints (Engineering)
|= ^A1031343
|
650 |
|
0 |
|a Joints (Engineering)
|
650 |
|
0 |
|a Strength of materials
|= ^A1064978
|
650 |
|
0 |
|a Strength of materials
|
650 |
|
7 |
|a Aluminum alloys
|x Fatigue
|2 fast
|0 http://id.worldcat.org/fast/806320
|
650 |
|
7 |
|a Aluminum alloys
|x Fatigue
|2 fast
|
650 |
|
7 |
|a Bolted joints
|x Testing
|2 fast
|0 http://id.worldcat.org/fast/835747
|
650 |
|
7 |
|a Bolted joints
|x Testing
|2 fast
|
650 |
|
7 |
|a Joints (Engineering)
|2 fast
|0 http://id.worldcat.org/fast/983929
|
650 |
|
7 |
|a Joints (Engineering)
|2 fast
|
650 |
|
7 |
|a Strength of materials
|2 fast
|0 http://id.worldcat.org/fast/1134837
|
650 |
|
7 |
|a Strength of materials
|2 fast
|
700 |
1 |
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|a Eaton, I. D.,
|e author
|
700 |
1 |
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|a Holt, M
|q (Marshall),
|e author.
|1 http://viaf.org/viaf/169049165
|
700 |
1 |
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|a Holt, M
|q (Marshall),
|e author.
|= ^A2733830
|
710 |
1 |
|
|a United States
|b National Advisory Committee for Aeronautics,
|e issuing body.
|1 http://viaf.org/viaf/136563305
|
710 |
1 |
|
|a United States
|b National Advisory Committee for Aeronautics,
|e issuing body.
|= ^A107111
|
776 |
0 |
8 |
|i Paper version:
|a Hartmann, E. C.,
|t Additional static and fatigue tests of high-strength aluminum-alloy bolted joints
|w (OCoLC)671811375
|
830 |
|
0 |
|a Technical note (United States. National Advisory Committee for Aeronautics) ;
|v 3269
|= ^A2720598
|
830 |
|
0 |
|a Technical note (United States. National Advisory Committee for Aeronautics) ;
|v 3269
|
999 |
1 |
0 |
|i 9a4c530c-72d2-4e08-a973-4117f4f9cef0
|l a13694980
|s US-CST
|m additional_static_and_fatigue_tests_of_high_strength_aluminum_alloy_bo_____1954_______natioa________________________________________hartmann__e__c_____________________y_3_n_21_5_6_3269e
|
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1 |
0 |
|i 9a4c530c-72d2-4e08-a973-4117f4f9cef0
|l 12381202
|s US-ICU
|m additional_static_and_fatigue_tests_of_high_strength_aluminum_alloy_bo_____1954_______natioa________________________________________hartmann__e__c_____________________y_3_n_21_5_6_3269e
|
999 |
1 |
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|b 13694980-1001
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