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mig00004935835 |
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OCoLC |
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20160302141918.0 |
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120213e199612 dcua obt f000 0 eng c |
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|a NAS 1.15:4770
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|a Online Government Document
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1 |
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|a Ko, William L.,
|e author.
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1 |
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|a Thermal and mechanical buckling analysis of hypersonic aircraft hat-stiffened panels with varying face sheet geometry and fiber orientation /
|c William L. Ko.
|
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|a [Washington, D.C.] :
|b National Aeronautics and Space Administration, Office of Management, Scientific and Technical Information Program,
|c December 1996.
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300 |
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|a 1 online resource (v, 30 pages) :
|b illustrations.
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336 |
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|a text
|b txt
|2 rdacontent
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|a computer
|b c
|2 rdamedia
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|a online resource
|b cr
|2 rdacarrier
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|a NASA technical memorandum ;
|v 4770
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500 |
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|a Title from title screen (viewed March 2, 2016).
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|a "December 1996."
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|a Includes bibliographical references (page 15).
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650 |
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7 |
|a Aircraft structures.
|2 nasat
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|
7 |
|a Thermal buckling.
|2 nasat
|
650 |
|
7 |
|a Mechanical properties.
|2 nasat
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650 |
|
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|a Finite element method.
|2 nasat
|
650 |
|
7 |
|a Hypersonic aircraft.
|2 nasat
|
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1 |
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|a United States.
|b National Aeronautics and Space Administration.
|b Scientific and Technical Information Program,
|e issuing body.
|
776 |
0 |
8 |
|i Print version:
|a Ko, William L.
|t Thermal and mechanical buckling analysis of hypersonic aircraft hat-stiffened panels with varying face sheet geometry and fiber orientation
|w (OCoLC)36171323
|
776 |
0 |
8 |
|i Microfiche version:
|a Ko, William L.
|t Thermal and mechanical buckling analysis of hypersonic aircraft hat-stiffened panels with varying face sheet geometry and fiber orientation
|w (OCoLC)37958339
|
830 |
|
0 |
|a NASA technical memorandum ;
|v 4770.
|
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|a 3342643
|b 06-10-21
|c 09-19-16
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|a DWS
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|a Middle Tennessee State University
|b Main
|c James E. Walker Library
|d Electronic Resources
|t 0
|e NAS 1.15:4770
|h Library of Congress classification
|
856 |
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|u http://purl.fdlp.gov/GPO/gpo65666
|z CONNECT
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