The behavior of fabric-film laminates under uniaxial and biaxial loading

AIAA International Balloon Technology Conference, 1999

Volumn , Issue , 1999, Pages 2-11

  Said, Magdi A ^a  

^a NASA GODDARD SPACE FLIGHT CENTER   (United States)

Author keywords

Crosshead displacement; Dynamic loading; Equilibrium conformations; Segmental motion; Stiffness; Stress relaxation; Ultimate load; Visco elasticity

Indexed keywords

CHARACTERIZATION; COMPOSITE FILMS; DYNAMIC LOADS; FILMS; LAMINATES; NASA; PLASTICS INDUSTRY; SOUNDING ROCKETS; STIFFNESS; STRENGTH OF MATERIALS; STRESS ANALYSIS; STRESS RELAXATION; TEXTILES; WEAVING;

CROSSHEAD DISPLACEMENT; DYNAMIC LOADINGS; EQUILIBRIUM CONFORMATION; SEGMENTAL MOTION; ULTIMATE LOADS;

LAMINATED COMPOSITES;

EID: 84976552925     PISSN: None     EISSN: None     Source Type: Conference Proceeding    
DOI: 10.2514/6.1999-3861     Document Type: Conference Paper

References (7)

1. Morris A. L., Scientific Ballooning Handbook, NCAR Technical Note/IA-99, 1975.
2. Needleman H. C., Nock R. S., Bawcom D. W., Status of the NASA Balloon Program, The 28th Plenary Meetings of COSPAR, Hague, Netherlands, July 1990.
3. Munson J.B., Preliminary Design Report for the long Duration Platform (LDP) Balloon Sheldahl, Inc., Advanced Products Division, Northfield, Minnesota, SER 0204, May 1975.
4. Said M. A., Mechanical Behavior of Polyester Non-woven Composite Films, Journal of Plastic Film & Sheeting, Vol. 13-July 1997.
5. Said M. A., and Thomas V., Proceedings of the ANTEC 1995, S.P.E. Technical Paper, Vol. 41, no.2, pp. 2419-2423, 1995
6. th Aerospace Sciences Meeting & Exhibit January 15-18, 1996/Reno,NV.
7. ASTM D 5035-90; Standard Test Method for Breaking Force and Elongation of Textile Fabrics (Strip Force)