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00000nam a22000007a 4500 |
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b2525841 |
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19960117095414.0 |
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he |||||||||| |
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960117s1995 vau b f000 0 eng d |
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|a (OCoLC)ocm34041795
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|a (GPO)96063504
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|a N 95-28817
|b NASA
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|a GPO
|c GPO
|d DLC
|d MvI
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|a COD9
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074 |
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|a 0830-H-14 (MF)
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086 |
0 |
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|a NAS 1.26:4676
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0 |
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|a NAS 1.26:4676
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245 |
0 |
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|a Effect of open hole on tensile failure properties of 2D triaxial braided textile composites and tape equivalents
|h [microform] /
|c Timothy L. Norman [and others]
|
260 |
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|a Hampton, Va. :
|b National Aeronautics and Space Administration, Langley Research Center ;
|a [Springfield, Va.] :
|b [National Technical Information Service, distributor],
|c [1995]
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300 |
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|a 1 volume.
|
336 |
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|a text
|b txt
|2 rdacontent.
|
337 |
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|a microform
|b h
|2 rdamedia.
|
338 |
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|a microfiche
|b he
|2 rdacarrier.
|
490 |
1 |
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|a NASA contractor report ;
|v 4676.
|
500 |
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|a Distributed to depository libraries in microfiche.
|
500 |
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|a Shipping list number: 96-0033-M.
|
533 |
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|a Microfiche.
|b [Washington, D.C. :
|c National Aeronautics and Space Administration,
|d 1995]
|e 1 microfiche.
|
650 |
|
7 |
|a Braided composites.
|2 nasat.
|
650 |
|
7 |
|a Crack initiation.
|2 nasat.
|
650 |
|
7 |
|a Crack propagation.
|2 nasat.
|
650 |
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7 |
|a Failure analysis.
|2 nasat.
|
650 |
|
7 |
|a Notch sensitivity.
|2 nasat.
|
650 |
|
7 |
|a Notch strength.
|2 nasat.
|
650 |
|
7 |
|a Notches.
|2 nasat.
|
650 |
|
7 |
|a Tensile strength.
|2 nasat.
|
650 |
|
7 |
|a Textiles.
|2 nasat.
|
700 |
1 |
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|a Norman, Timothy L.
|0 http://id.loc.gov/authorities/names/no2009122888.
|
710 |
2 |
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|a Langley Research Center.
|0 http://id.loc.gov/authorities/names/n79134855
|1 http://isni.org/isni/0000000406376754.
|
830 |
|
0 |
|a NASA contractor report ;
|v NASA CR-4676.
|0 http://id.loc.gov/authorities/names/n83825229.
|
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|a .b25258412
|b 03-18-20
|c 02-14-96
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|a gov
|b 02-14-96
|c -
|d m
|e -
|f eng
|g vau
|h 0
|i 1
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|a .b25258412
|b 11-23-14
|c 02-14-96
|
944 |
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|a MARS - RDA ENRICHED
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907 |
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|a .b25258412
|b 12-19-08
|c 02-14-96
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|a .b25258412
|b 02-14-96
|c 02-14-96
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