PROCEEDINGS VOLUME 3994
SPIE'S 5TH ANNUAL INTERNATIONAL SYMPOSIUM ON NONDESTRUCTIVE EVALUATION AND HEALTH MONITORING OF AGING INFRASTRUCTURE | 6-8 MARCH 2000
Nondestructive Evaluation of Aging Aircraft, Airports, and Aerospace Hardware IV
IN THIS VOLUME

0 Sessions, 23 Papers, 0 Presentations
Session I  (7)
Session II  (3)
Session III  (6)
Session IV  (7)
SPIE'S 5TH ANNUAL INTERNATIONAL SYMPOSIUM ON NONDESTRUCTIVE EVALUATION AND HEALTH MONITORING OF AGING INFRASTRUCTURE
6-8 March 2000
Newport Beach, CA, United States
Session I
Proc. SPIE 3994, Low-frequency electromagnetic technique for nondestructive evaluation, 0000 (5 May 2000); doi: 10.1117/12.385014
Proc. SPIE 3994, Reduced order computational methodology for damage detection in structures, 0000 (5 May 2000); doi: 10.1117/12.385022
Proc. SPIE 3994, Detection of cracks in multilayer aircraft structures with fasteners using remote field eddy current method, 0000 (5 May 2000); doi: 10.1117/12.385030
Proc. SPIE 3994, Eddy current measurements with magneto-resistive sensors: third-layer flaw detection in a wing-splice structure 25 mm thick, 0000 (5 May 2000); doi: 10.1117/12.385032
Proc. SPIE 3994, Nondestructive evaluation of aircraft structure using lock-in thermography, 0000 (5 May 2000); doi: 10.1117/12.385033
Proc. SPIE 3994, Role of data fusion in NDE for aging aircraft, 0000 (5 May 2000); doi: 10.1117/12.385034
Proc. SPIE 3994, Feasibility of optical interference-based NDE methods to inspect helicopter rotor blades, 0000 (5 May 2000); doi: 10.1117/12.385035
Session II
Proc. SPIE 3994, Ultrasonic detection of corrosion between riveted plates, 0000 (5 May 2000); doi: 10.1117/12.385036
Proc. SPIE 3994, Optical device based on thermoplastic recording, 0000 (5 May 2000); doi: 10.1117/12.385015
Session III
Proc. SPIE 3994, Acoustic emission structural health management systems (AE-SHMS), 0000 (5 May 2000); doi: 10.1117/12.385016
Proc. SPIE 3994, Durability patch and damage dosimeter: a portable battery-powered data acquisition computer and durability patch design process, 0000 (5 May 2000); doi: 10.1117/12.385017
Proc. SPIE 3994, Fusion of modal strain energy for health monitoring of aircraft structures, 0000 (5 May 2000); doi: 10.1117/12.385018
Proc. SPIE 3994, Transversely loaded fiber optic grating strain sensors for aerospace applications, 0000 (5 May 2000); doi: 10.1117/12.385019
Proc. SPIE 3994, Applying thermoelasticity to impact-damaged structural components, 0000 (5 May 2000); doi: 10.1117/12.385020
Session IV
Proc. SPIE 3994, Nondestructive evaluation of crack propagation under a composite patch repair using the eddy current method, 0000 (5 May 2000); doi: 10.1117/12.385021
Proc. SPIE 3994, Ultrasonic evaluation of co-cured composite structures, 0000 (5 May 2000); doi: 10.1117/12.385023
Proc. SPIE 3994, Near Lamb mode imaging of multilayered composite plates, 0000 (5 May 2000); doi: 10.1117/12.385024
Proc. SPIE 3994, Effects of exciting frequencies, grain sizes, and damage upon P-wave velocity for ultrasonic NDT of concrete, 0000 (5 May 2000); doi: 10.1117/12.385025
Proc. SPIE 3994, Evaluating pavement layer properties with a high-speed rolling deflectometer, 0000 (5 May 2000); doi: 10.1117/12.385026
Proc. SPIE 3994, Ultrasonic materials evaluation of automotive inflator components, 0000 (5 May 2000); doi: 10.1117/12.385027
Session III
Proc. SPIE 3994, Eddy current technique applied to the nondestructive evaluation of turbine blade wall thickness, 0000 (5 May 2000); doi: 10.1117/12.385028
Session IV
Proc. SPIE 3994, Detection of cracks near sharp edges by using giant magneto-resistance-based eddy current probe, 0000 (5 May 2000); doi: 10.1117/12.385029
Session II
Proc. SPIE 3994, Technology assessment of MEMS for NDE and condition-based maintenance, 0000 (5 May 2000); doi: 10.1117/12.385031
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