| Tag |
First Indicator |
Second Indicator |
Subfields |
| LEADER |
00000cam a2200000Ia 4500 |
| 001 |
in00002665607 |
| 005 |
20211202193918.0 |
| 006 |
m d f |
| 007 |
cr cn||||||||| |
| 008 |
100727s2005 vaua ob f000 0 eng d |
| 035 |
|
|
|a (OCoLC)ocn650359265
|
| 040 |
|
|
|a GPO
|c GPO
|d MvI
|d UtOrBLW
|
| 049 |
|
|
|a WWW
|
| 074 |
|
|
|a 0830-D (online)
|
| 086 |
0 |
|
|a NAS 1.15:2005-213932
|
| 100 |
1 |
|
|a Thornburgh, Robert P.
|
| 245 |
1 |
0 |
|a Identifying and characterizing discrepancies between test and analysis results of compression-loaded panels /
|c Robert P. Thornburgh, Mark W. Hilburger.
|
| 264 |
|
1 |
|a Hampton, Va. :
|b National Aeronautics and Space Administration, Langley Research Center,
|c [2005]
|
| 300 |
|
|
|a 1 online resource (29 pages) :
|b illustrations
|
| 336 |
|
|
|a text
|b txt
|2 rdacontent
|
| 337 |
|
|
|a computer
|b c
|2 rdamedia
|
| 338 |
|
|
|a online resource
|b cr
|2 rdacarrier
|
| 490 |
1 |
|
|a NASA TP- ;
|v 2005-213932
|
| 500 |
|
|
|a Title from title screen (viewed on July 27, 2010).
|
| 500 |
|
|
|a "October 2005."
|
| 500 |
|
|
|a "ARL-TR-3664."
|
| 504 |
|
|
|a Includes bibliographical references (pages 12-13).
|
| 536 |
|
|
|h 23-064-30-30.
|
| 500 |
|
|
|a Electronic resource.
|
| 650 |
|
7 |
|a Compression loads.
|2 nasat
|
| 650 |
|
7 |
|a Panels.
|2 nasat
|
| 650 |
|
7 |
|a Mathematical models.
|2 nasat
|
| 650 |
|
7 |
|a Structural analysis.
|2 nasat
|
| 650 |
|
7 |
|a Fabrication.
|2 nasat
|
| 700 |
1 |
|
|a Hilburger, Mark W.
|
| 710 |
2 |
|
|a Langley Research Center.
|
| 830 |
|
0 |
|a NASA technical paper ;
|v 213932.
|
| 856 |
4 |
0 |
|u https://purl.fdlp.gov/GPO/LPS124600
|t 0
|
| 999 |
|
|
|a MARS
|
| 999 |
f |
f |
|s a4c1c03b-4407-3dff-94bf-821833f40388
|i ebca5bdb-48c7-3746-bf3e-423f281e3948
|t 0
|
| 952 |
f |
f |
|a Texas A&M University
|b College Station
|c Electronic Resources
|d Available Online
|t 0
|e NAS 1.15:2005-213932
|h Superintendent of Documents classification
|
| 998 |
f |
f |
|a NAS 1.15:2005-213932
|t 0
|l Available Online
|