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| 001 |
0a825ff3-54ed-4cf7-99eb-851cf6d1a242 |
| 005 |
20240705000000.0 |
| 008 |
960815s1995 vau b f000 0 eng d |
| 035 |
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|a (OCoLC)35248054
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| 037 |
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|a N 96-18070
|b NASA
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| 040 |
|
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|a GPO
|c GPO
|d DLC
|d MvI
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| 049 |
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|a [MF] MNUJ
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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 1.26:198253
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| 099 |
|
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|a NAS 1.26:198253
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| 100 |
1 |
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|a Mikulas, Martin M.
|
| 245 |
1 |
2 |
|a A new merit function for evaluating the flaw tolerance of composite laminates /
|c Martin M. Mikulas, Jr., and Rod Sumpter.
|
| 260 |
|
|
|a Hampton, Va. :
|b National Aeronautics and Space Administration, Langley Research Center ;
|a [Springfield, Va.] :
|b [National Technical Information Service, distributor],
|c [1995]
|
| 300 |
|
|
|a 1 volume.
|
| 336 |
|
|
|a text
|b txt
|2 rdacontent
|
| 337 |
|
|
|a microform
|b h
|2 rdamedia
|
| 338 |
|
|
|a microfiche
|b he
|2 rdacarrier
|
| 490 |
1 |
|
|a NASA contractor report ;
|v 198253
|
| 500 |
|
|
|a Distributed to depository libraries in microfiche.
|
| 500 |
|
|
|a Shipping list no.: 96-0467-M.
|
| 533 |
|
|
|a Microfiche.
|b [Washington, D.C. :
|c National Aeronautics and Space Administration,
|d 1996]
|e 1 microfiche.
|
| 650 |
|
7 |
|a Aerospace engineering.
|2 nasat
|
| 650 |
|
7 |
|a Design analysis.
|2 nasat
|
| 650 |
|
7 |
|a Fault tolerance.
|2 nasat
|
| 650 |
|
7 |
|a High strength.
|2 nasat
|
| 650 |
|
7 |
|a Impact damage.
|2 nasat
|
| 650 |
|
7 |
|a Laminates.
|2 nasat
|
| 650 |
|
7 |
|a Materials tests.
|2 nasat
|
| 650 |
|
7 |
|a Orthotropism.
|2 nasat
|
| 700 |
1 |
|
|a Sumpter, Rod.
|
| 710 |
2 |
|
|a Langley Research Center.
|
| 830 |
|
0 |
|a NASA contractor report ;
|v NASA CR-198253.
|
| 999 |
1 |
0 |
|i 0a825ff3-54ed-4cf7-99eb-851cf6d1a242
|l 9950211330001701
|s US-MNU
|m new_merit_function_for_evaluating_the_flaw_tolerance_of_composite_lami_____1995_______natioa________________________________________mikulas__martin_m__________________nas_1_26_198253p
|