JAMS 2006 Annual Technical Review Meeting

Dates:
Tuesday, June 20, 2006 – Thursday, June 22, 2006
Hosted by:
Center of Excellence for Advanced Materials in Transport Aircraft Structures (AMTAS)
Location:
University of Washington, 220 Kane Hall; Seattle, WA

The Center of Excellence for Advanced Materials in Transport Aircraft Structures (AMTAS) is hosting the FAA Joint Advanced Materials and Structures (JAMS) Center of Excellence 2006 Technical Meeting.

This meeting will be the second annual technical peer review of the research in progress for JAMS. The purpose of this meeting is to showcase the JAMS research in composites, advanced structures and crashworthiness.

Attendees will be provided with background information on the research tasks prior to the meeting. The technical review will consist of presentations from the Principal Investigators in AMTAS and the Center of Excellence for Composites and Advanced Materials (CECAM), the two groups which make up JAMS and the FAA Materials and Structures Branch.

Professionals from the aviation community will also be presenting. This review will help JAMS and the FAA focus their research efforts appropriately to the needs of the aviation industry.

The objectives of this technical review are to:

  1. Review the research of the JAMS Center of Excellence and FAA Materials and Structures in composites, advanced structures and crashworthiness.
  2. Access current industry practice and compare that to the current research areas.
  3. Recommend additional research activities.

Tuesday, June 20, 2006

Time
Presenter
Title
1:15 pm
Curtis DaviesFAA JAMS Program Manager
Introduction to FAA Research
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1:45 pm
Jim BrownToray Composites (America), Inc.
Industry Presentation: Toray Composites (America), Inc.
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2:00 pm
Shreeram RajCytec Engineered Materials
Industry Presentation: Cytec Engineered Materials
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2:15 pm
Jason ScharfC&D Zodiac
Industry Presentation: C&D Zodiac
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2:30 pm
Andrew WalkerUniversity of Manchester
Composite Education in the UK
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3:00 pm
Larry IlcewiczFAA
Course Development: Maintenance of Composite Aircraft Structures
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3:40 pm
Gerardo OlivaresWichita State University
Crashworthiness Certification by Analysis: Numerical Model Preparation and Analysis Guidelines
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4:20 pm
Hyonny KimPurdue University
Damage Tolerance and Durability of Adhesively Bonded Composite Structures
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Wednesday, June 21, 2006

Time
Presenter
Title
8:00 am
Dirk HeiderUniversity of Delaware
VARTM Variability and Substantiation
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8:40 am
Development of Reliability-Based Damage Tolerant Structural Design Methodology
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9:20 am
Sridhar KrishnaswamyNorthwestern University
Structural Health Monitoring for Life Management of Aircraft
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10:20 am
Suresh (Raju) KeshavanarayanaWichita State University
Full-Scale Damage Tolerance of Sandwich Structures
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11:00 am
J.M. YangUCLA
Damage Tolerance and Durability of Fiber Metal Laminates for Aircraft Structures
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12:45 pm
Eli Livne, Ph.D.University of Washington Aeronautics and Astronautics
Combined Global/Local Variability and Uncertainty in Integrated Aeroservoelasticity of Composite Aircraft
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1:25 pm
Bill StevensonWichita State University
Quantifying Methods for the Evaluation of the Fitness of Fiber Reinforced Composite Surfaces for Subsequent Adhesive Bonding
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2:05 pm
Brian Flinn, Ph.D.University of Washington Materials Science & Engineering
Improving Adhesive Bonding of Composites through Surface Characterization
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3:00 pm
Lloyd Smith, Ph.D.Washington State University School of Mechanical & Materials EngineeringPrashanthi PothakamuriWashington State University
The Effect of Surface Treatment on the Degradation of Composite Adhesives
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3:40 pm
Identification and Validation of Analytical Chemistry Methods for Detecting Composite Surface Contamination and Moisture
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4:20 pm
Lamia SalahWichita State University
Effects of Repair Procedures Applied to Composite Airframe Structures
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Thursday, June 22, 2006

Time
Presenter
Title
8:00 am
Yeow NgWichita State University
Production Control Effect on Composite Material Quality and Stability
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8:40 am
Lamia SalahWichita State University
Aging Effects Evaluation of a Beechcraft Starship and a Decommissioned Boeing CRFP 737-200 Horizontal Stabilizer
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9:20 am
Suresh (Raju) KeshavanarayanaWichita State University
Crashworthiness of Composite Fuselage Structures—Material Dynamic Properties
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10:15 am
Christian WidenerWichita State University
Evaluation of Friction Stir Weld Process and Properties for Aerospace Application
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10:55 am
Andy ThomasBell Helicopter Textron
Industry Feedback: Bell Helicopter Textron
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11:45 am
Jim KroneCessna Aircraft Company
Industry Feedback: Cessna Aircraft Company
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Time
Presenter
Title
JAMS 2006 Research Project Summaries
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