Structural Health Monitoring and Integrity Management
Latest Publications

TOTAL DOCUMENTS

124

(FIVE YEARS 0)

H-INDEX

1

(FIVE YEARS 0)

Published By CRC Press

9780429226472

Latest Documents Most Cited Documents Contributed Authors Related Sources Related Keywords

The inspection for Shipbuilding Gantry Cranes’ managing system of safety monitoring

Structural Health Monitoring and Integrity Management ◽

10.1201/b18510-96 ◽

2015 ◽

pp. 297-300

Keyword(s):

Safety Monitoring ◽

Managing System ◽

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Structural Health Monitoring and Integrity Management ◽

10.1201/b18510-95 ◽

2015 ◽

pp. 296-296

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we bolted BGK-FBG-4150 sensors on wireless strain sensors on the specimen the specimen instead of welding on it, with 502 plastic. This four kinds of we pasted MOI FBG sensors on the sensors are arranged in the middle specimen with the help of AB glue, and position of the specimen in order to we pasted FLA-5-11 strain sensor and ensure the unity, as shown in Fig.1;

Structural Health Monitoring and Integrity Management ◽

10.1201/b18510-94 ◽

2015 ◽

pp. 292-295

Keyword(s):

Strain Sensor ◽

Strain Sensors ◽

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Analysis of safety status and risk factors of supercritical power station boiler

Structural Health Monitoring and Integrity Management ◽

10.1201/b18510-90 ◽

2015 ◽

pp. 277-280

Keyword(s):

Risk Factors ◽

Power Station ◽

Power Station Boiler

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Structural Health Monitoring and Integrity Management ◽

10.1201/b18510-89 ◽

2015 ◽

pp. 276-276

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Session 4: Prognosis of damage and health management

Structural Health Monitoring and Integrity Management ◽

10.1201/b18510-86 ◽

2015 ◽

pp. 269-269

Keyword(s):

Health Management

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Material eect in normal beam EMAT Non-Destructive Testing

Structural Health Monitoring and Integrity Management ◽

10.1201/b18510-85 ◽

2015 ◽

pp. 265-268

Keyword(s):

Non Destructive Testing ◽

Destructive Testing ◽

Non Destructive

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were designed to explore the factors that affect the ( 0.3)(W h0.264) resonant frequency. Strain measurement was (3) achieved by bonding the antenna to a cantilever beam and applying loads at the free end of the canti-Assuming that the antenna is subjected to a ten-lever beam, and microstrip antenna sensors that can sile strain ε along its electrical length direction, detect the crack length and propagtion alng diffr-the patch width and the su bstrate thickness will ent orientation with a sub-millimeter resolution was change due to Poisson’s effect, i.e., discussed.

Structural Health Monitoring and Integrity Management ◽

10.1201/b18510-82 ◽

2015 ◽

pp. 256-260

Keyword(s):

Resonant Frequency ◽

Crack Length ◽

Cantilever Beam ◽

Strain Measurement ◽

Microstrip Antenna ◽

Electrical Length ◽

Length Direction ◽

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Session 1: Advanced sensing technology

Structural Health Monitoring and Integrity Management ◽

10.1201/b18510-8 ◽

2015 ◽

pp. 17-17 ◽

Keyword(s):

Sensing Technology

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Study on fatigue crack monitoring of metallic aircraft structure based on attached eddy current sensor

Structural Health Monitoring and Integrity Management ◽

10.1201/b18510-77 ◽

2015 ◽

pp. 239-245

Keyword(s):

Fatigue Crack ◽

Eddy Current ◽

Current Sensor ◽

Aircraft Structure ◽

Eddy Current Sensor ◽

Crack Monitoring

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