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01016nam a2200217 a 4500 |
| 001 |
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20171111230504.0 |
| 008 |
081126s1980 gr r 000 0 eng d |
| 040 |
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|a GR-KoDPT
|b gre
|e AACR2
|
| 100 |
1 |
|
|a Davis, Randall C.
|
| 245 |
1 |
0 |
|a Stress analysis and buckling of J-stiffened graphite-epoxy panel/
|c Randall C. Davis
|
| 260 |
|
|
|a Washington:
|b National Aeronautics and Space Administration, Scientific and Technical Information Office,
|c 1980
|
| 300 |
|
|
|a 20 σ. :
|b ill ;
|c 27 εκ.
|
| 490 |
0 |
|
|a NASA technical paper
|v 1607
|
| 650 |
|
0 |
|a Epoxy compounds
|x Testing
|
| 650 |
|
0 |
|a Laminated materials
|x Testing
|
| 650 |
|
0 |
|a Buckling (Mechanics)
|x Testing
|
| 710 |
|
|
|a United States
|b National Aeronautics and Space Administration
|b Scientific and Technical Information Office
|
| 710 |
0 |
|
|a United States.
|b National Aeronautics and Space Administration.
|b Scientific and Technical Information Office
|
| 710 |
2 |
|
|a Langley Research Center
|
| 952 |
|
|
|a GR-KoDPT
|b 59cc204f6c5ad13446f87f3e
|c 998a
|d 945l
|e TL 521 .3
|t 1
|x m
|z Books
|
