An Approximate solution and master curves for buckling of symmetrically laminated composite cylinders /

Bibliographic Details
Main Author: Nemeth, Michael P. (Author)
Corporate Author: United States. National Aeronautics and Space Administration (sponsoring body.)
Format: Government Document eBook
Language:English
Published: Hampton, Virginia : National Aeronautics and Space Administration, Langley Research Center, 2013.
Series:NASA technical memorandum ; 217999.
Subjects:
Online Access:https://purl.fdlp.gov/GPO/gpo45682
http://purl.fdlp.gov/GPO/gpo45682

MARC

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074 |a 0830-D (online) 
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100 1 |a Nemeth, Michael P.,  |e author. 
245 1 3 |a An Approximate solution and master curves for buckling of symmetrically laminated composite cylinders /  |c Michael P. Nemeth. 
264 1 |a Hampton, Virginia :  |b National Aeronautics and Space Administration, Langley Research Center,  |c 2013. 
300 |a 1 online resource (60 pages) :  |b color 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/TM ;  |v 2013-217999 
500 |a Title from title screen (viewed on Feb. 12, 2014). 
500 |a "May 2013." 
504 |a Includes bibliographical references (page 19). 
536 |a Sponsored by the National Aeronautics and Space Administration  |h 869021.04.07.01.13 
536 |d ; L-20250 
650 7 |a Anisotropy.  |2 nasat 
650 7 |a Axial compression loads.  |2 nasat 
650 7 |a Cylindrical shells.  |2 nasat 
650 7 |a Inhomogeneity.  |2 nasat 
650 7 |a Laminates.  |2 nasat 
650 7 |a Sandwich structures.  |2 nasat 
710 2 |a Langley Research Center,  |e issuing body. 
710 1 |a United States.  |b National Aeronautics and Space Administration,  |e sponsoring body. 
830 0 |a NASA technical memorandum ;  |v 217999. 
856 4 0 |u https://purl.fdlp.gov/GPO/gpo45682  |t 0 
856 4 0 |u http://purl.fdlp.gov/GPO/gpo45682  |t 0 
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