Reflections on Jim Starnes' technical contributions

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

Volumn 2, Issue , 2005, Pages 845-850

  Haftka, Raphael T ^a,b  

^a UNIVERSITY OF FLORIDA   (United States)

^b Department of Mechanical and Aerospace Engineering ^*  (United States)

Author keywords

[No Author keywords available]

Indexed keywords

COMPOSITE MATERIALS; PROBLEM SOLVING; RESEARCH;

AEROSPACE RESEARCHERS; GOVERNMENT LABORATORIES; RESEARCH COLLABORATORS; UNIVERSITIES;

AEROSPACE ENGINEERING;

EID: 28844484546     PISSN: 02734508     EISSN: None     Source Type: Conference Proceeding    
DOI: 10.2514/6.2005-1872     Document Type: Conference Paper

References (15)

1. Acar, E., Haftka, R.T., Sankar, B.V. and Qui, X. "Increasing Design Load and Reducing Weight of Structures by Error Reduction," to be presented at the 45th AIAA/ASME/ASCE/AHS/ASC Structures, Structural Dynamics, and Materials Conference, Austin, Texas, 18-21 April 2005.
2. Arbocz, Johann; and Starnes, James H., Jr.: On a High-Fidelity Hierarchical Approach to Buckling Load Calculations. In "Calladine Festschrift," S. Pellegrino, Ed., Wolters Kluwer Academic Publishers. Dordrecht, The Netherlands, 2002.
3. Haftka, R. T. and Starnes, J. H., Jr., "Stiffness Tailoring for Improved Compressive Strength of Composite Plates with Holes," AIAA Journal, Vol. 26, No. 1, pp. 72-77, 1988.
4. Le Riche, R. and Haftka, R.T., "Optimization of Laminate Stacking Sequence for Buckling Load Maximization by Genetic Algorithm," AIM Journal, 31 (5), pp. 951-956, 1993.
5. Li, Yi-Wei; Elishakoff, Isaac; Starnes, James H., Jr.; and Bushnell, David: Effect of the Thickness Variation and Initial Imperfection on Buckling of Composite Cylindrical Shells: Asymptotic Analysis and Numerical Results by BOSOR4 and PANDA2. International Journal of Solids and Structures, Vol. 34, No. 28, 1997, pp. 3755-3767.
6. Nagendra, S., Haftka, R. T., Gürdal, Z., and Starnes, J. H., "Design of Stiffened Composite Plate with a Hole," Composite Structures, Vol. 18, pp. 195-219, 1991.
7. Nagendra, S., Jestin, D., Gürdal, Z., Haftka, R.T., and Watson, L.T., "Improved genetic Algorithms for the Design of Stiffened Composite Panels," Computers & Structures, Vol. 58, No. 3, pp. 543-555, 1996.
8. Noor, A. K.; Starnes, J. H., Jr.; and Peters, J. P.: Mechanics of Postbuckling of Multilayered Composite Panels with a Cutout. Composite Structures, Vol. 30, No. 4, 1995, pp. 369-388.
9. Park, O., Haftka, R.T., Sankar, B.V., Starnes, J.H., and Nagendra, S., "Analytical-Experimental Correlation for a Stiffened Composite Panel Loaded in Axial Compression," Journal of Aircraft, 38 (2), 379-387, 2001.
10. Prasad, Chunchu B.; Ambur, Damodar R.; and Starnes, James H., Jr.: Response of Laminated Composite Plates to Low-Speed Impact by Different Impactors. AIAA Journal, Vol. 32, No, 6, June 1994, pp. 1270-1277.
11. Qu, X., Haftka, R.T., Venkataraman, S., and Johnson, T.F., "Deterministic and Reliability-Based Optimization of Composite Laminates for Propellant Tanks," AIAA Journal, 41(10), pp. 2029-2036, 2003.
12. Rhodes, Marvin D.; Williams, Jerry G.; and Starnes, James H., Jr.: Low-Velocity Impact Damage in Fiber-Reinforced Laminated Epoxy Structures. Polymer Composites, Vol. 2, No. 1, January 1981, pp. 36-44.
13. Schultz, W., Smarslok, B., Speriatu, L., Ifju, P.G. and Haftka, R.T., "Residual Stress Determination Using Temperature Dependent Material Properties and Uncertainty Analysis," to be presented at the SEM Annual Conference and Exposition, Portland OR, June 7-9, 2005.
14. Starnes, J. H., Jr. and Haftka, R.T., "Preliminary Design of Composite Wings for Buckling, Strength and Displacement Constraints," Journal of Aircraft, Vol. 16 (8), pp. 564-570, 1979.
15. Starnes, James H., Jr.; Knight, Norman F., Jr.; and Rouse, Marshall: Postbuckling Behavior of Selected Flat Stiffened Graphite-Epoxy Panels Loaded in Compression. AIM Journal, Vol. 23, No. 8, August 1985, pp. 1236-12