Non-deterministic optimization of composite structures reliability

Collection of Technical Papers - AIAA/ASME/ASCE/AHS/ASC Structures, Structural Dynamics and Materials Conference

Volumn 5, Issue , 2004, Pages 4071-4081

  Abumeri, Galib H ^a   Chamis, Christos C ^b  

^a QSS GROUP INC   (United States)

^b NASA GLENN RESEARCH CENTER   (United States)

Author keywords

[No Author keywords available]

Indexed keywords

AEROSPACE STRUCTURES; COMPOSITE FUSELAGE; COMPOSITE MECHANICS; DAMAGE PROGRESSION;

AEROSPACE ENGINEERING; ALGORITHMS; COMPUTATIONAL METHODS; COMPUTER SIMULATION; FUSELAGES; PROBABILITY; RELIABILITY THEORY; STRUCTURAL ANALYSIS; STRUCTURAL OPTIMIZATION;

COMPOSITE STRUCTURES;

EID: 16244367104     PISSN: 02734508     EISSN: None     Source Type: Conference Proceeding    
DOI: None     Document Type: Conference Paper

References (5)

1. Murthy, P.L.N. and Chamis, C.C.: ICAN: Integrated Composites Analyzer. Journal of Composites Technology & Research, 1986, Vol. 8, No. 1, pp. 8-17.
2. th Structures, Structural Dynamics and Materials Conference, pp. 1174-1186, 1993.
3. Probabilistic Structural Analysis Methods (PSAM) for Select Space Propulsion Systems Components, NESSUS/FPI Theoretical Manual, Southwest Research Institute, NASA Contract NAS3-24389, Dec. 1989.
4. Minnetyan, L, Chamis, C.C., and Abdi, F.: Damage Tolerance of Fiber Composite Airfoils with Piezoelectric Adaptive Control System. AIAA 2000-1504. CD ROM, April 2000.
5. Progressive Failure Analysis for 2D/3D Laminate/Woven/Braided/Stitched Polymer and Ceramic Matrix Composite (GENOA Software Release 3.2, 2004) Alpha Star Corporation, Long Beach, CA.