A system of monitoring vibration of a blasting model test for a jointed rock mass and a method are provided. The system includes: a loading subsystem for three-way load, a model-surface blasting-vibration acquisition subsystem, and a model-interior dynamic stress-strain acquisition subsystem. The system and the method are provided, and a blasting model for a transparent jointed rock mass and a monitoring method that are obtained can analyze the influence of a joint inclination angle on propagation and attenuation laws of blasting stress waves in the jointed rock mass, and can analyze the influence of different millisecond blasting modes on the stability of an existing tunnel in the jointed rock mass, and can capture a real-time dynamic evolution process of cracks. The stress and strain measurement technologies used can perform omnibearing monitoring and recording for large deformations of surrounding rock under blasting load, and can resist the electromagnetic interference.

A displacement measurement system enables accurate and easy measurement of the maximum displacement formed on plates which are used for military or civil purposes, especially in vehicle manufacture, and which are subjected to a blast or crash test.

A displacement measurement system enables accurate and easy measurement of the maximum displacement formed on plates which are used for military or civil purposes, especially in vehicle manufacture, and which are subjected to a blast or crash test.

An apparatus and a method for simulating a mechanical stress applied to a sealant from a lightning strike upon an aircraft is provided. The apparatus comprises a specimen, a test fixture, and a capacitor. The specimen comprises an electrically non-conductive sealant for an aircraft fuel tank having a cylindrical shape, and an electrically conductive wire centered axially within the sealant. The test fixture secures the specimen during testing. The capacitor is electrically coupled to the test fixture, and simulates a lightning strike upon the aircraft by vaporizing the wire with a current to generate a mechanical shock to the sealant.

An apparatus and a method for simulating a mechanical stress applied to a sealant from a lightning strike upon an aircraft is provided. The apparatus comprises a specimen, a test fixture, and a capacitor. The specimen comprises an electrically non-conductive sealant for an aircraft fuel tank having a cylindrical shape, and an electrically conductive wire centered axially within the sealant. The test fixture secures the specimen during testing. The capacitor is electrically coupled to the test fixture, and simulates a lightning strike upon the aircraft by vaporizing the wire with a current to generate a mechanical shock to the sealant.

A process for vibration analysis, including the steps of: receiving synchronized motion measurements of particle motion in two or three orthogonal dimensions over a selected period of time at a plurality of different measurement locations; and determining one or more strain waveforms in the orthogonal dimensions in regions spanning the plurality of measurement locations using the motion measurements.

A process for vibration analysis, including the steps of: receiving synchronized motion measurements of particle motion in two or three orthogonal dimensions over a selected period of time at a plurality of different measurement locations; and determining one or more strain waveforms in the orthogonal dimensions in regions spanning the plurality of measurement locations using the motion measurements.

Multiple test coupons are incorporated in the construction of a personal garment for the purpose of determining the presence of foreign substances acquired during garment use or a change in properties or other change in characteristics over time. Each of the test coupons is retained with the garment during the useful life of the garment until the coupon is individually removed for test purposes. Each test coupon has a construction identical to the garment construction and is easily removable and configured to allow for destructive testing. Sufficient multiple coupons are provided with each garment over its life to allow for periodic testing.

Multiple test coupons are incorporated in the construction of a personal garment for the purpose of determining the presence of foreign substances acquired during garment use or a change in properties or other change in characteristics over time. Each of the test coupons is retained with the garment during the useful life of the garment until the coupon is individually removed for test purposes. Each test coupon has a construction identical to the garment construction and is easily removable and configured to allow for destructive testing. Sufficient multiple coupons are provided with each garment over its life to allow for periodic testing.

A multiple energetic penetration and damage progression sensor is disclosed. A grid of sensing lines, such as passive optical fibers, is formed by laying the sensing lines in a crossing pattern to form a 2-Dimensional or 3-Dimensional coordinate grid. Signal receivers such as photo-detectors are connected to one or both ends of the sensing lines, and a data processor interprets received signals. When an impact or energetic penetration occurs at a location on or near a sensing line, energy passes down the sensing line in both directions away from the point of impact or penetration. Each pair of X-Y or X-Y-Z recordings from receivers receiving the energy is processed to determine a location, penetration volume and progression in time of the impact or penetration. This sensor can be made conformal to any regular and continuous surface geometry, volume geometry, or surfaces or volumes of physical objects of interest.