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

Bibliographic Details
Uniform Title:NASA technical memorandum ; 4770.
Main Author: Ko, William L.
Corporate Author: United States. National Aeronautics and Space Administration. Scientific and Technical Information Program
Language:English
Published: [Washington, DC] : [Springfield, Va.] : National Aeronautics and Space Administration, Office of Management, Scientific and Technical Information Program ; [National Technical Information Service, distributor], 1996.
Series:NASA technical memorandum ; 4770.
Subjects:
Physical Description:1 volume.
Format: Government Document Microfilm Book

MARC

LEADER 00000nam a2200000Ka 4500
001 in00002191154
003 OCoLC
005 20220616042625.0
007 he ||||||||||
008 971118s1996 dcu b f000 0 eng d
035 |a (OCoLC)37958339 
037 |a N 97-13249  |b NASA 
040 |a GPO  |c GPO  |d DLC  |d MvI  |d UtOrBLW 
049 |a QEMX 
074 |a 0830-D (MF) 
086 0 |a NAS 1.15:4770 
099 |a NAS 1.15:4770 
100 1 |a Ko, William L.  |0 http://id.loc.gov/authorities/names/n82045659 
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. 
260 |a [Washington, DC] :  |b National Aeronautics and Space Administration, Office of Management, Scientific and Technical Information Program ;  |a [Springfield, Va.] :  |b [National Technical Information Service, distributor],  |c 1996. 
300 |a 1 volume. 
336 |a text  |b txt  |2 rdacontent 
337 |a microform  |b h  |2 rdamedia 
338 |a microfiche  |b he  |2 rdacarrier 
490 1 |a NASA technical memorandum ;  |v 4770 
500 |a Distributed to depository libraries in microfiche. 
500 |a Shipping list number: 97-0960-M. 
500 |a Microform. 
533 |a Microfiche.  |b [Washington, D.C. :  |c National Aeronautics and Space Administration,  |d 1997]  |e 1 microfiche. 
650 7 |a Aircraft structures.  |2 nasat 
650 7 |a Panels.  |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 
650 7 |a Fiber orientation.  |2 nasat 
710 1 |a United States.  |b National Aeronautics and Space Administration.  |b Scientific and Technical Information Program.  |0 http://id.loc.gov/authorities/names/no91017593 
830 0 |a NASA technical memorandum ;  |v 4770.  |0 http://id.loc.gov/authorities/names/n83707893 
907 |y .b32954542  |b 211113  |c 980610 
998 |a (2)gd  |a 7f  |b 980604  |c m  |d a   |e -  |f eng  |g dcu  |h 0  |i 2 
935 |a .b16124005LM  |b 04-10-98  |c 04-10-98 
935 |a BER3348 
999 f f |i f9052960-0bb5-5ded-802a-8deef1937f4d  |s 381d3961-a00e-50a2-b601-53fa3f4cdddd  |t 0 
952 f f |p Non-Circulating  |a Michigan State University-Library of Michigan  |b Michigan State University  |c MSU Government Documents  |d MSU Government Documents - U.S. Fiche, 2 West  |t 0  |e NAS 1.15:4770  |h Other scheme  |i Microform (Microfilm/Microfiche)  |n 1