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050202s1981 gr r f000 0 eng d |
| 040 |
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|a GR-KoDPT
|b gre
|e AACR2
|
| 100 |
1 |
|
|a Anthony, Frank M.
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| 245 |
1 |
0 |
|a Design and fabrication of a stringer stiffened discrete tube actively cooled panel for a hypersonic aircraft/
|c Frank M. Anthony and Robert G. Helenbrook ; prepared for Langley Research Center under contract NAS1-12806
|
| 260 |
|
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|a Washington, D.C.:
|b National Aeronautics and Space Administration, Scientific and Technical Information Branch,
|c 1981
|
| 300 |
|
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|a ix, 79 σ. :
|b εικ. ;
|c 27 εκ.
|
| 490 |
0 |
|
|a NASA contractor report
|v NASA CR-3403
|
| 500 |
|
|
|a "February 1981."
|
| 504 |
|
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|a Περιέχει βιβλιογραφικές παραπομπές
|
| 650 |
|
0 |
|a Thermal stresses
|
| 700 |
1 |
|
|a Helenbrook, Robert G.
|
| 710 |
|
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|a United States
|b National Aeronautics and Space Administration
|b Scientific and Technical Information Branch
|
| 710 |
0 |
|
|a United States.
|b National Aeronautics and Space Administration.
|b Scientific and Technical Information Branch
|
| 710 |
0 |
|
|a Langley Research Center
|
| 952 |
|
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|a GR-KoDPT
|b 59cc2e6c6c5ad13446fa9769
|c 998a
|d 945l
|e TL 521 .3
|t 1
|x m
|z Books
|
