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Minimum-mass design of filamentary composite panels under combined loads : design procedure based on a rigorous buckling analysis /

中图分类法 :
TH12
著者:
Stroud, W.Fefferson.
题名:
Minimum-mass design of filamentary composite panels under combined loads [design procedure based on a rigorous buckling analysis ]
出版发行:
Washington : National aeronautics and space administration, 1977.
载体形态:
48 p. : ill. ; 29 cm.
丛编:
NASA Technical Note NAS TN D-8417.
主要责任者:
Agranoff, Nancy.
主要责任者:
Anderson, Meivin S.
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HEA|  |00847nam  2200205 a 450 
001|  |021997015161
005|  |20050713123250.0
008|  |050610s1976    waua     b    000 0 eng
040|  |▼aWHUT▼cWHUT
093|  |▼aTH12▼23
100|1 |▼aStroud, W.Fefferson.
245|10|▼aMinimum-mass design of filam-
   |  |entary composite panels under -
   |  |combined loads :▼bdesign proce-
   |  |dure based on a rigorous buckl-
   |  |ing analysis /▼cW.Jefferson St-
   |  |rouD,Nancy Agranoff,Meivin S.Anderson.
260|  |▼aWashington :▼bNational aeron-
   |  |autics and space administration,▼c1977.
300|  |▼a48 p. :▼bill. ;▼c29 cm.
440| 0|▼aNASA Technical Note NAS TN D-8417.
504|  |▼aIncludes bibliographical references.
700|1 |▼aAgranoff, Nancy.
700|1 |▼aAnderson, Meivin S.
950|  |▼aJ▼fTH12/S925
999|  |▼tE▼Atshs21▼a20050712 10:12:12-
   |  |▼Gtshs11▼g20050614 08:31:12▼Mt-
   |  |shs21▼m20050713 12:32:52
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