Thermal and mechanical buckling analysis of hypersonic aircraft hat-stiffened panels with varying face sheet geometry and fiber orientation /

Saved in:
Bibliographic Details
Main Author: Ko, William L. (Author)
Format: Government Document Electronic eBook
Language:English
Published: [Washington, D.C.] : National Aeronautics and Space Administration, Office of Management, Scientific and Technical Information Program, December 1996.
Series:NASA technical memorandum ; 4770.
Subjects:
Online Access:CONNECT

MARC

LEADER 00000nam a2200000 i 4500
001 mig00004935835
003 OCoLC
005 20160302141918.0
006 m o d f
007 cr bn|||||||||
008 120213e199612 dcua obt f000 0 eng c
035 0 0 |a ocn777248062 
040 |a OCLCE  |b eng  |e rda  |e pn  |c OCLCE  |d OCLCQ  |d OCLCO  |d GPO  |d MvI 
042 |a pcc 
049 |a TXME 
074 |a 0830-D (online) 
086 0 |a NAS 1.15:4770 
099 |a Online Government Document 
100 1 |a Ko, William L.,  |e author. 
245 1 0 |a Thermal and mechanical buckling analysis of hypersonic aircraft hat-stiffened panels with varying face sheet geometry and fiber orientation /  |c William L. Ko. 
264 1 |a [Washington, D.C.] :  |b National Aeronautics and Space Administration, Office of Management, Scientific and Technical Information Program,  |c December 1996. 
300 |a 1 online resource (v, 30 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 technical memorandum ;  |v 4770 
500 |a Title from title screen (viewed March 2, 2016). 
500 |a "December 1996." 
504 |a Includes bibliographical references (page 15). 
650 7 |a Aircraft structures.  |2 nasat 
650 7 |a Thermal buckling.  |2 nasat 
650 7 |a Mechanical properties.  |2 nasat 
650 7 |a Finite element method.  |2 nasat 
650 7 |a Hypersonic aircraft.  |2 nasat 
710 1 |a United States.  |b National Aeronautics and Space Administration.  |b Scientific and Technical Information Program,  |e issuing body. 
776 0 8 |i Print version:  |a Ko, William L.  |t Thermal and mechanical buckling analysis of hypersonic aircraft hat-stiffened panels with varying face sheet geometry and fiber orientation  |w (OCoLC)36171323 
776 0 8 |i Microfiche version:  |a Ko, William L.  |t Thermal and mechanical buckling analysis of hypersonic aircraft hat-stiffened panels with varying face sheet geometry and fiber orientation  |w (OCoLC)37958339 
830 0 |a NASA technical memorandum ;  |v 4770. 
856 4 0 |z CONNECT  |u http://purl.fdlp.gov/GPO/gpo65666  |t 0 
907 |a 3342643  |b 06-10-21  |c 09-19-16 
998 |a wi  |b 09-19-16  |c m  |d z   |e -  |f eng  |g dcu  |h 0  |i 1 
910 |a MTSUM(2016)2,3,4,5,6,8 
910 |a DWS 
999 f f |i 76b6f99d-0589-4f67-9577-a16dbc899665  |s deca7815-4b13-4935-86b7-686e268a76a6  |t 0 
952 f f |a Middle Tennessee State University  |b Main  |c James E. Walker Library  |d Electronic Resources  |t 0  |e NAS 1.15:4770  |h Library of Congress classification 
856 4 0 |t 0  |u http://purl.fdlp.gov/GPO/gpo65666  |z CONNECT