JOURNALS
A. Trego, et al, 2003,
“A Scientific Approach to Side Underride Analysis,” Advances
in Vehicle Aggressivity and Compatability, Side and Rear Impact and Rollover
Protection,
SP-1775, Society of Automotive Engineers, Warrendale, PA, SAE Technical
Paper No. 2003-01-0178, pp. 41-47, 2003.
A. Trego, et al, 2003, “A Scientific Approach to Side Underride Analysis,” Advances in Vehicle Aggressivity and Compatability, Side and Rear Impact and Rollover Protection, SP-1775, Society of Automotive Engineers, Warrendale, PA, SAE Technical Paper No. 2003-01-0178, pp. 41-47, 2003.
A.
Trego et al, 2001, “Analysis
of Side Underride Crashes Misconceptions and the Problems,” Accident
Investigation Quarterly, Issue 27, Summer 2001, pp. 17-19.
Peer Reviewed JOURNALS
A.
Trego and D. Cope, 2001, “Evaluation
of DaDT Lap Joint Analysis Tools,” AIAA
Journal, Vol. 39, No. 12, pp. 2250-2254.
Peer
Reviewed Conferences
S.
Calvert, et al, 2004, “High Density Distributed Sensing Methods Using
Fiber Bragg Gratings to Measure Structural Damage in Adhesive Bonds and
Aircraft Structures,” The Air Force Research Laboratory Integrated
Systems Health Management Conference, Dayton, Ohio. August 2004.
A. Trego, 2004, “Structural Health Monitoring Technology on Commercial Aircraft II,” European Workshop on Structural Health Monitoring, Munich, Germany. July 2004.
C. Greenberg et al, 2004, “Structural Health Monitoring Technology on Commercial Aircraft,” Seventh International Aerospace Corrosion Control Symposium, Amsterdam, Holland. April 2004.
A. Trego, 2003, “Installation of the Autonomous Structural Integrity Monitoring System,” International Workshop on Structural Health Monitoring, San Francisco, CA. September 2003.
A. Akdeniz et al, 2003, “Structural Health Management (SHM) Technology Implementation on Commercial Airplanes,” Sixth Joint DoD/FAA/NASA Conference on Aging Aircraft Proceedings, New Orleans, LA. September 2003.
A. Trego, 2003, “An Update on Monitoring Moisture Ingression with Fiber Optic Sensors,” Sixth Pacific Northwest Fiber Optic Workshop, Troutdale, Oregon. May 2003.
A. Trego, 2003, “Monitoring Moisture Ingression with Fiber Optic Sensors,” Sixth International Conference on Sandwich Structures, Ft. Lauderdale, Florida. March 2003.
J. Elster, et al, 2003,
“Flight Demonstration of Fiber Optic Sensors,” SPIE’s
International Symposium on Nondestructive Evaluation Techniques for Aging
Infrastructure & Manufacturing Conference
Proceedings,
A. Trego, and D. Smith, 2002, “Battery Operated Health Monitoring System,” Fifth Joint DoD/FAA/NASA Conference on Aging Aircraft Proceedings, San Francisco, California.
D. Banaszak, et al, 2002,
“Damage Dosimeter Third Octave and Time History RMS Values,” Joint Statistical Meeting 2002, New
York, NY. August 2002.
D. Banaszak, et al, 2002,
“A Quick Look at
Flight Data from a Digital Damage Dosimeter,” ESTECH
2002 Environmental Sciences and Technology, Anaheim,
CA. May 2002.
A. Trego, R. Keller, 2002, “Fiber
Optics in Bonded Repairs,”
SAMPE 2002 International Symposium & Exhibition, Long
Beach,
E.
Haugse, et al, 2001, “Optical Fiber-Based Health Monitoring Systems for
Composite Structures,” Third International Workshop on Structural
Health Monitoring, Stanford, CA,
2001.
A.
Trego, et al, 2001, “Optical Fiber-Based Health Monitoring Systems for
Composite Structures,” AIAC
Australian International Aerospace Congress, Canberra, ACT, Australia
2001.
J.
Elster, et al, 2001, “Optical Fiber-Based Adhesive Bondline Monitoring
Systems for Composite Patch Systems,” SPIE’s
International Symposium on Nondestructive Evaluation Techniques for Aging
Infrastructure & Manufacturing Conference
Proceedings, Newport Beach California. March 2001.
J.
Elster, M. Jones, P. Tuloa, A. Trego, and I. Perez, 2000, “Corrosion Monitoring in Aging Aircraft Using Optical Fiber-Based
Chemical Sensors,” Fourth Joint DoD/FAA/NASA
Conference on Aging Aircraft Proceedings, St. Louis, Missouri, pp.
13-20.
W.
Schulz, E. Udd, J. Seim, I. Perez, and A. Trego, 2000, “Progress on Health
Monitoring of An Adhesive Joint Using a Multi-Axis Fiber Grating Strain
Sensor System,” SPIE’s International Symposium on Nondestructive Evaluation Techniques
for Aging Infrastructure & Manufacturing Conference Proceedings, Vol. 3991-9, Newport Beach California.
E.
Udd, et al, 2000, “Use of Transversely Loaded Fiber Grating Strain Sensors
for Aerospace Applications,” SPIE’s
International Symposium on Nondestructive Evaluation Techniques for Aging
Infrastructure & Manufacturing Conference
Proceedings, Vol. 3994-17, Newport Beach California.
E.
Udd, et al, 2000, “Multidimensional Strain Field Measurements Using Fiber
Optic Grating Sensors,” SPIE’s
International Symposium on Nondestructive Evaluation Techniques for Aging
Infrastructure & Manufacturing Conference
Proceedings, Vol. 3986-35, Newport Beach California.
W.
Schulz, E. Udd, M. Morrell, J. Seim, I. Perez, and A. Trego, 1999, “Health
Monitoring of an Adhesive Joint Using a Multi-Axis Fiber Grating Strain
Sensor System,” SPIE’s International Symposium on Nondestructive Evaluation Techniques
for Aging Infrastructure & Manufacturing Conference Proceedings, Vol. 3586, Newport Beach California, pp.
41-52.
A.
Berens, D. West and A. Trego, 1999, “Risk
Assessment of Fatigue Cracks in Corroded Lap Joints,” RTO
Applied Vehicle Technology Panel Meeting
Proceedings 18: Fatigue in the
Presence of Corrosion, Cedex, France, pp. 21-1 – 21-10.
D.
Cope, A. Trego, and D. West, 1999, “Analytical
Framework for Assessment of Corrosion and Fatigue in Fuselage Lap Joints,”
Second Joint NASA/FAA/DoD Conference
on Aging Aircraft Proceedings
NASA/CP-1999-208982/Part1, Williamsburg, Virginia, pp. 472 – 481.
A.
Trego, E. Haugse and E. Udd, 1998, “Material
Removal Rate Fiber Optic Corrosion Sensor,” Fourth
Pacific Northwest Fiber Optic Sensor Workshop Proceedings
of SPIE, Vol. 3489, Troutdale, Oregon, pp. 105-109.
A.
Trego, et al, 1998, “Analytical
Methodology for Assessing Corrosion and Fatigue in Fuselage Lap Joints,” 1998
Air Force Corrosion Program Conference Proceedings, Macon, Georgia.
PresentatiONS
A. Trego, 2004, “Structural Health Management: An Overview of Current
Research Efforts at Boeing,” ASM Aeromat Conference, Seattle,
Washington.
K. Cooper, et al, 2004, “Fiber Optic Sensor System for Aircraft Health
Monitoring,” ASM Aeromat Conference, Seattle, Washington.
A. Trego, 2004, “Autonomous Structural Integrity Monitoring System for
Environmental Conditions,” CPAC Conference, Seattle, Washington.
Invited Presentation.
A. Trego, 2004, “Autonomous Structural Integrity Monitoring System for
Environmental Conditions,” CHTE Conference, Seattle, Washington.
A. Trego, 2003, “Autonomous Structural Integrity Monitoring System,”
DASCON Conference, Seattle, Washington.
R. Ikegami, A. Trego, 2002, “Battery Operated Health Monitoring System,”
DASCON Conference, St. Louis, Missouri.
R.
Ikegami, E. Haugse, and A. Trego, 2001, “Structural Monitoring for Damped
Composite Repairs,” ASM Aeromat Conference, Long Beach, California.
A.
Trego and T. Leeks, 2000, “Damage Detection Techniques Through The Use Of
Acoustic Emissions,” ASM Aeromat Conference, Seattle, Washington. Outstanding Technical Presentation
Award.
R.
Ikegami and A. Trego, 2000, “Structural Health Management: An Overview of
Current Research Efforts at Boeing,” ASM
Aeromat Conference, Seattle, Washington.
E.
Udd, W. Schulz, J. Seim, I. Perez, A. Trego, E. Haugse, 2000, “Nondestructive
Evaluation of Adhesive Joints Using Advanced Fiber Grating Strain Sensor
Technology,” ASM Aeromat Conference, Seattle, Washington.
A.
Trego, 2000, “The Use of Fiber Optic Sensors for Health Monitoring of
Bonded Repair Structures,” Fifth
Pacific Northwest Fiber Sensor Workshop, Troutdale, Oregon.
E.
Udd, W. Schulz, M. Morrell, J. Seim, I. Perez, A. Trego, 1999, “Structural
Health Monitoring of an Adhesive Joint Using a Multi-Axis Fiber Grating
Strain Sensor System,” ASM Aeromat Conference, Dayton, Ohio.
Peer Reviewed JOURNALS
A.
Trego et al, 2003, “Axial Passive Damping Testing of Mass-Produced Stress
Coupled, Co-cured Damped Composites,” AIAA
Journal Vol. 41, No. 3 pp. 512-516.
A.
Trego and P. Eastman, 1999, “Flexural Damping Predictions of Mechanical
Elements Designed Using Stress Coupled, Co-cured Damped Fiber Reinforced
Composites,” Journal of Advanced Materials, Vol. 31, No. 1, pp. 7- 17.
A.
Trego and P. Eastman, 1997, “Optimization
of Passively Damped Composite Structures,” International Journal of
Modelling & Simulation, Vol. 17, No. 4, pp. 284-288.
A.
Trego, D. Olcott, and P. Eastman, 1997, “Improved Axial Damping of
Mechanical Elements Through the Use of Multiple Layered, Stress Coupled,
Co-cured Damped Fiber Reinforced Composites,” Journal
of Advanced Materials, Vol. 28, No. 2, pp. 28-34.
PresentatiONS
Angela
Trego, 1995, “Improved Structural Damping of Mechanical Elements Through
the Use of Multiple Layered, Stress Coupled, Co-cured Damped Fiber
Reinforced Composites,” SAMPE ’95
International SAMPE Symposium & Exhibition, Anaheim, California.
First place: SAMPE National
Student Competition for Ph. D. Division.
Peer
Reviewed Conferences
A.
Trego, P. Eastman, W. Pratt, and C. Jensen, 1995, “Reduced Boring Bar
Vibrations Using Damped Composite Structures,” Proceedings
of the 1995 Design Engineering Technical Conferences, Vol. 3, Part A,
pp. 305-311.
A.
Trego, P. Eastman, and C. Jensen, 1995, “Optimization of Passively Damped Composite
Structures,”
Proceedings
of the IASTED International Conference on Applied Modelling, Simulation and
Optimization, pp. 137-141.
PresentatiONS
A.
Trego, and K. Chase, 1993, “AutoCATS User’s Manual,” Association
for the Development of Computer Aided Tolerancing Systems (ADCATS),
Brigham Young University, Provo, Utah.
Angela
Trego, 1993, “Tolerance Analysis,” SAMPE
’95 International SAMPE Symposium & Exhibition, Anaheim,
California. First place: SAMPE National Student Competition for M. S.
Division.