Stephen Tsai
Professor (Research) of Aeronautics and Astronautics, Emeritus
Bio
Professor Tsai's research interest is in the development of design methodology of composite materials and structures. As an emerging technology, composite materials offer unique performances for structures that combine light weight with durability. Keys to the successful utilization of composite materials are predictability in performance and cost effective design of anisotropic, laminated structures. Current emphasis is placed on the understanding of failure modes, and computer simulation for design and cost estimation.
Academic Appointments
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Emeritus Faculty, Acad Council, Aeronautics and Astronautics
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Member, Cardiovascular Institute
Boards, Advisory Committees, Professional Organizations
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Member, National Academy of Engineering (1995 - Present)
2023-24 Courses
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Independent Studies (2)
- Directed Research and Writing in Aero/Astro
AA 190 (Sum) - Independent Study in Aero/Astro
AA 199 (Sum)
- Directed Research and Writing in Aero/Astro
All Publications
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Buckling optimization of Double-Double (DD) laminates with gradual thickness tapering
COMPOSITE STRUCTURES
2025; 351
View details for DOI 10.1016/j.compstruct.2024.118568
View details for Web of Science ID 001318313100001
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Topology optimization of Double-Double (DD) composite laminates considering stress control
COMPUTER METHODS IN APPLIED MECHANICS AND ENGINEERING
2023; 414
View details for DOI 10.1016/j.cma.2023.116191
View details for Web of Science ID 001029211300001
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Defining the Design Space for Double-Double Laminates by Considering Homogenization Criterion
AIAA JOURNAL
2023
View details for DOI 10.2514/1.J062639
View details for Web of Science ID 000946604300001
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Double-Double: New Family of Composite Laminates
AIAA JOURNAL
2021; 59 (11): 4293-4305
View details for DOI 10.2514/1.J060659
View details for Web of Science ID 000729172000002
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Design of laminates by a novel "double-double'' layup
THIN-WALLED STRUCTURES
2021; 165
View details for DOI 10.1016/j.tws.2021.107954
View details for Web of Science ID 000661248500004
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Application of the Tsai's modulus and double-double concepts to the definition of a new affordable design approach for composite laminates
COMPOSITE STRUCTURES
2021; 259
View details for DOI 10.1016/j.compstruct.2020.113246
View details for Web of Science ID 000609377400009
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D and DD-drop layup optimization of aircraft wing panels under multi-load case design environment
COMPOSITE STRUCTURES
2020; 248
View details for DOI 10.1016/j.compstruct.2020.112518
View details for Web of Science ID 000552864700005
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A novel invariant-based design approach to carbon fiber reinforced laminates
COMPOSITE STRUCTURES
2017; 159: 44-52
View details for DOI 10.1016/j.compstruct.2016.09.055
View details for Web of Science ID 000386759100005
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A trace-based approach to design for manufacturing of composite laminates
JOURNAL OF REINFORCED PLASTICS AND COMPOSITES
2016; 35 (7): 589-600
View details for DOI 10.1177/0731684415624770
View details for Web of Science ID 000373944600006
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A unit circle failure criterion for carbon fiber reinforced polymer composites
COMPOSITES SCIENCE AND TECHNOLOGY
2016; 123: 71-78
View details for DOI 10.1016/j.compscitech.2015.12.011
View details for Web of Science ID 000370095100009
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Trace-based stiffness for a universal design of carbon-fiber reinforced composite structures
COMPOSITES SCIENCE AND TECHNOLOGY
2015; 118: 23-30
View details for DOI 10.1016/j.compscitech.2015.08.003
View details for Web of Science ID 000364254100004
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An invariant-based theory of composites
COMPOSITES SCIENCE AND TECHNOLOGY
2014; 100: 237-243
View details for DOI 10.1016/j.compscitech.2014.06.017
View details for Web of Science ID 000340222400032
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Smart cure of thick composite filament wound structures to minimize the development of residual stresses
EUROMECH 453 Colloquium on Internal Stresses in Polymer Composite Processing and Service Life
ELSEVIER SCI LTD. 2006: 530–37
View details for DOI 10.1016/j.compositesa.2005.05.017
View details for Web of Science ID 000236338500003
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Three decades of composites activities at US Air Force Materials Laboratory
COMPOSITES SCIENCE AND TECHNOLOGY
2005; 65 (15-16): 2295-2299
View details for DOI 10.1016/j.compscitech.2005.05.017
View details for Web of Science ID 000233076100003
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Time- and temperature-dependent failures of a metal-to-composites bonded joint with PMMA adhesive material
JOURNAL OF COMPOSITE MATERIALS
2003; 37 (1): 35-54
View details for DOI 10.1106/002199803028993
View details for Web of Science ID 000180309200003
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A progressive quadratic failure criterion, part B
COMPOSITES SCIENCE AND TECHNOLOGY
2002; 62 (12-13): 1683-1695
View details for Web of Science ID 000177970200013
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PECVD silicon carbide as a chemically resistant material for micromachined transducers
9th International Conference on Solid-State Sensors and Actuators
ELSEVIER SCIENCE SA. 1998: 48–55
View details for Web of Science ID 000075835900007
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A progressive quadratic failure criterion for a laminate
COMPOSITES SCIENCE AND TECHNOLOGY
1998; 58 (7): 1023-1032
View details for Web of Science ID 000076342100004
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Obituary: Late Professor Tsuyoshi Hayashi
ADVANCED COMPOSITE MATERIALS
1998; 7 (3): 217-218
View details for Web of Science ID 000075585200004
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Analysis and behavior of grid structures
COMPOSITES SCIENCE AND TECHNOLOGY
1996; 56 (9): 1001-1015
View details for Web of Science ID A1996VR25500001
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SCHOOLING TAIWAN WOMEN - EDUCATIONAL-ATTAINMENT IN THE MID-20TH CENTURY
Meeting of the Research-Committee-on-Social-Stratification of the International-Sociological-Association
AMER SOCIOLOGICAL ASSOC. 1994: 243–63
View details for Web of Science ID A1994QY44300003