PROCEEDINGS VOLUME 3586
NONDESTRUCTIVE EVALUATION TECHNIQUES FOR AGING INFRASTRUCTURES AND MANUFACTURING | 3-5 MARCH 1999
Nondestructive Evaluation of Aging Aircraft, Airports, and Aerospace Hardware III
IN THIS VOLUME

0 Sessions, 37 Papers, 0 Presentations
NONDESTRUCTIVE EVALUATION TECHNIQUES FOR AGING INFRASTRUCTURES AND MANUFACTURING
3-5 March 1999
Newport Beach, CA, United States
Health Monitoring I
Proc. SPIE 3586, AACE: an innovative partnership to enhance aircraft safety, 0000 (28 January 1999); doi: 10.1117/12.339874
Proc. SPIE 3586, Corrosion quantification by different nondestructive inspection methods, 0000 (28 January 1999); doi: 10.1117/12.339881
Proc. SPIE 3586, Nondestructive evaluation for crack, corrosion, and stress detection for metal assemblies and structures, 0000 (28 January 1999); doi: 10.1117/12.339888
Proc. SPIE 3586, Crack growth detection and monitoring using broadband acoustic emission techniques, 0000 (28 January 1999); doi: 10.1117/12.339897
Proc. SPIE 3586, Health monitoring of an adhesive joint using a multiaxis fiber grating strain sensor system, 0000 (28 January 1999); doi: 10.1117/12.339906
Proc. SPIE 3586, Structural damage localization using an optimization method, 0000 (28 January 1999); doi: 10.1117/12.339908
Health Monitoring II
Proc. SPIE 3586, Nondestructive characterization of corrosion damage and fatigue life, 0000 (28 January 1999); doi: 10.1117/12.339909
Proc. SPIE 3586, Developments in real-time 2D ultrasound inspection for aging aircraft, 0000 (28 January 1999); doi: 10.1117/12.339910
Proc. SPIE 3586, Aircraft engine blade cooling holes detection and classification from infrared images, 0000 (28 January 1999); doi: 10.1117/12.339875
Proc. SPIE 3586, State of the art of thermal wave imaging for NDE of aging aircraft, 0000 (28 January 1999); doi: 10.1117/12.339876
Proc. SPIE 3586, Three-dimensional CT data processing for inspection, 0000 (28 January 1999); doi: 10.1117/12.339877
NDE of Airport and Aerospace Hardware
Proc. SPIE 3586, Use of noncontact sensors for paving operations on airport pavements, 0000 (28 January 1999); doi: 10.1117/12.339878
Proc. SPIE 3586, Monitoring crack length in concrete beams using resonance measurements, 0000 (28 January 1999); doi: 10.1117/12.339879
Proc. SPIE 3586, High-speed rolling deflectometer data evaluation, 0000 (28 January 1999); doi: 10.1117/12.339880
Proc. SPIE 3586, Nondestructive critical pressure determination of defect zones in vessel-like constructions, 0000 (28 January 1999); doi: 10.1117/12.339882
Proc. SPIE 3586, Low-frequency electromagnetic sensing of cracks and inclusions in ferromagnetic materials using magnetoresistive sensors, 0000 (28 January 1999); doi: 10.1117/12.339883
Proc. SPIE 3586, Improved near-field characteristics of phased arrays for assessing concrete and cementitious materials, 0000 (28 January 1999); doi: 10.1117/12.339884
Emerging NDE Technologies
Proc. SPIE 3586, Log-periodic time-to-failure analysis, 0000 (28 January 1999); doi: 10.1117/12.339885
Proc. SPIE 3586, Fusion of modal strain energy differences for localization of damage, 0000 (28 January 1999); doi: 10.1117/12.339886
Proc. SPIE 3586, Damage detection in a stiffened plate using modal strain energy differences, 0000 (28 January 1999); doi: 10.1117/12.339887
Proc. SPIE 3586, NUVU: handheld instruments for video inspection of aircraft wiring, 0000 (28 January 1999); doi: 10.1117/12.339889
Proc. SPIE 3586, Pulse phase thermography for defect detection and visualization, 0000 (28 January 1999); doi: 10.1117/12.339890
Proc. SPIE 3586, Real-time speckle shearography system for defect detection in aircraft materials, 0000 (28 January 1999); doi: 10.1117/12.339891
Lamb Wave NDE
Proc. SPIE 3586, Composite materials stiffness determination and defects characterization using enhanced leaky Lamb wave dispersion data acquisition method, 0000 (28 January 1999); doi: 10.1117/12.339892
Proc. SPIE 3586, Residual stresses in aircraft components: I. Nonlinear finite element modeling, 0000 (28 January 1999); doi: 10.1117/12.339893
Proc. SPIE 3586, Residual stresses in aircraft components: II. Nondestructive characterization using leaky Lamb waves, 0000 (28 January 1999); doi: 10.1117/12.339894
Proc. SPIE 3586, Impact of damage on propagation of Lamb waves in plates, 0000 (28 January 1999); doi: 10.1117/12.339895
Proc. SPIE 3586, Ultrasonic Lamb wave tomographic scanning, 0000 (28 January 1999); doi: 10.1117/12.339896
Proc. SPIE 3586, Lamb wave tomographic imaging system for aircraft structural health assessment, 0000 (28 January 1999); doi: 10.1117/12.339898
Proc. SPIE 3586, Wide-area imaging of ultrasonic Lamb wave fields by electronic speckle pattern interferometry, 0000 (28 January 1999); doi: 10.1117/12.339899
Proc. SPIE 3586, Micromachined ultrasonic transducers for air-coupled nondestructive evaluation, 0000 (28 January 1999); doi: 10.1117/12.339900
Poster Session
Proc. SPIE 3586, Advanced radiographic methods for visualization of corrosion in aircraft structures, 0000 (28 January 1999); doi: 10.1117/12.339901
Proc. SPIE 3586, Emerging holographic techniques for advanced space research, 0000 (28 January 1999); doi: 10.1117/12.339902
Proc. SPIE 3586, NDE of hidden flaws in aging aircraft structures using obliquely backscattered ultrasonic signals (OBUS), 0000 (28 January 1999); doi: 10.1117/12.339903
Health Monitoring II
Proc. SPIE 3586, Precise AE source location technology for the aerospace industry, 0000 (28 January 1999); doi: 10.1117/12.339904
Emerging NDE Technologies
Proc. SPIE 3586, Recent advances in remote field eddy current NDE techniques and their applications in detection, characterization, and monitoring of deeply hidden corrosion in aircraft structures, 0000 (28 January 1999); doi: 10.1117/12.339905
Lamb Wave NDE
Proc. SPIE 3586, Surface detection with subvoxel accuracy using 3D directional derivatives, 0000 (28 January 1999); doi: 10.1117/12.339907
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