Wichita - 2005

TUESDAY

Sh
ear Characterization of Composite Laminates and Adhesives
Dr. Daniel O. Adams
The University of Utah


Composite Safety and Certification Initiatives
Larry Ilcewicz, Oregon State University

JAMS Technical Meeting Introduction

Structural Health Monitoring for Life Management of Aircraft
Northwestern University

VARTM Variability and Substantiation
University of Delaware Center for Composite Materials

Effects of Repair Procedures Applied to Composite Airframe Laminate Structures
Wichita State University 


WEDNESDAY

Course Development: Maintenance of Composite Aircraft Structures
Larry Illcewicz
Edmonds Community College

Fatigue Behavior of VARTM Manufactured Affordable 2x2 Biaxial Carbon Braided Composites
Ajit D. Kelkar and John D. Whitcomb
FAA Aviation Research- Materials and Structures Branch

Damage Tolerance and Durability of Adhesively Bonded Composite Structures
Hyonny Kim, Purdue University

Development of Reliability-Based Damage Tolerant Structural Design Methodology
Dr. Kuen Y. Lin, University of Washington

 Combined Global/Local Variability and Uncertainty in the Aeroservoelasticity of Composite Aircraft
Eli Livne, University of Washington

 Nanophased Skin-Stringer Assembly for Aircraft Structures
Hassan Mahfuz, Florida Atlantic University
Shaik Jeelani, Tuskegee University

Crashworthiness of Composites- Material Dynamic Properties
K.S. Raju, Wichita State University

Adhesive Characterization & Element Testing of Fatigued and Damaged Bonded Joints
Wichita State University
FAA Aviation Research

Laminate Statistical Design Allowable Generation for Fiber Reinforced Composite Materials
Wichita State University
FAA Aviation Research

Methods for the Evaluation of the Fitness of Fiber Reinforced Composite Surfaces for Subsequent Adhesive Bonding
Bill Stevenson, Wichita State University

Evaluation of Friction Stir Welding Processes and Properties for Aircraft Application
Bryan Tweedy
Wichita State University

Damage Tolerance and Durability of Fiber-Metal Laminates for Aircraft Structures
Jenn-Ming Yang, UCLA

Production Control Effect on Composite Material Quality and Stability
John Tomblin; Yeow Ng
Wichita State University

Identification and Validation of Analytical Chemistry Methods for Detecting Composite Surface Contamination and Moisture
Xiangyang Zhou, Florida International University
FAA Aviation Research

 

THURSDAY

Improving Adhesive Bonding of Composites through Surface Characterization
Brian D. Flinn
University of Washington

JAMS/CECAM Better Tools and Techniques
Gould
Baytheon Aircraft Company

Boeing Industry Perspective on the Presented Research
Daniel J. Hoffman; Alan G. Miller
Boeing Inc.

The Boeing 787 Dreamliner: More than an Airplane
Alan G. Miller; Daniel J. Hoffman

Joint Advanced Materials and Structures Center of Excellence Technical Meeting
Andy Kasowski
Cessna Inc.

Full-Scale Damage Tolerance of Sandwich Structures
K.S. Raju, Wichita State University

Aging Effects Evaluation of a Beechcraft Starship and a Decommissioned Boeing CRFP 737-200 Horizontal Stabilizer
Wichita State University

The Effect of Surface Treatment on the Degradation of Composite Adhesives
Lloyd Smith, Washington State University