Technical Publications
Over the years, the scientists at Alpha STAR
Corporation have authored numerous technical
publications, write-ups, and presentations
at various industry conferences across the United States.
Please click on any of the documents below to view immediately:
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Facesheet Delamination of Composite Sandwich Materials at Cryogenic Temperatures
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Risk Management of Composite Structure
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Collaborative Virtual Testing for manufacturing & Life Cycle Management
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Optimizing Composite Rocket Motor Development Using Advanced Evolutionary Algorithms
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Probabilistic Life Evaluation of Ceramic Matrix Composite Combustor Liner
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Probabilistic Impact Analysis and Risk Assessment Supporting Shuttle Return-To-Flight Procedures
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Fracture Mechanics of Ductile
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Durability and Damage Tolerance of Composites
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Progressive Fracture of Stitched Composite Shear in the Post Buckling Range
Technical References from Newsletters
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Development of MMPDS Handbook Aircraft Design Allowables.
Prepared for the 7th Joint DOD/FAA/NASA
Conference on Aging Aircraft, September
8-11, 2003, New Orleans, LA.
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Material Qualification and Equivalency for Polymer
Matrix Composite Material System: Updated
Procedure. Office of Aviation Research,
Washington, D.C. 20591, U.S. Department
of Transportation Federal Aviation Administration,
September, 2003.
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Obtaining A-Basis and B-Basis Allowable Values for
Open-Hole Specimens Using Virtual Testing.
AIAAC-2007-127, 4. Ankara International
Aerospace Conference, 10-12 September,
2007 - METU, Ankara.
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Simplified Analytical Procedure for Prediction of
Fracture Damage in Composite Structures.
ASTM COMMITTEE-D30 Symposium on Joining
and Repair of Composite Structure March
17-18, 2003 Kansas City, MO.
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Damage Tolerance of Laminated Tee Joints in FRP
Structures. Composites Part A - Applied
Science and Manufacturing, Vol. 29, No.
4, pp. 465, 1998.
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Progressive Failure Analysis of Shuttle Reinforced
Carbon-Carbon Plate Specimens. AIAA-2006-1789,
RI, May 1-5.
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Estimation of Fatigue and Fracture Allowables for
Metallic Materials Under Cyclic Loading.
AIAA-2007-2381.
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Probabilistic Fracture Toughness, Fatigue Crack Growth
Estimation Resulting From Material Uncertainties.
ASTM International Paper.
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Virtual Testing And Progressive Failure Analysis
of Army Composite Bridges. SAMPE 2004,
Long Beach, CA 2004.
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Composite army bridges under fatigue cyclic loading.
Journal of Society of Infrastructure Engineering
(SIE), Taylor and Francis Publications,
Vol 2, No 1. March, 2006, 63-73.
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Prediction of Micro-crack Densities in Cryogenic
IM7/977-2 Propellant Tanks. 45rd AIAA
Structures, Structural Dynamics, and Materials
Conference, AIAA-2006-1933.
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Prediction of Micro-crack Densities in IM7/977-2
Polymer Composite Laminates under Mechanical
Loading at Room and Cryogenic Temperatures.
46rd AIAA Structures, Structural Dynamics,
and Materials Conference, AIAA-2005-2226.
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Crack Growth Strategy in Composites under Static
Loading. 47th AIAA-2006-1842, Newport,
RI, May 1-5, 2006.
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Facesheet Delamination of Composite Sandwich Materials
at Cryogenic Temperatures. Journal
of Composite Science and Technology, 2006.
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