scholarly journals High speed volumetric thickness profile measurement based on full-field wavelength scanning interferometer

2008 ◽  
Vol 16 (25) ◽  
pp. 21022 ◽  
Author(s):  
Jang-Woo You ◽  
Soohyun Kim ◽  
Daesuk Kim
Keyword(s):  
High Speed ◽  
Profile Measurement ◽  
Full Field ◽  
Thickness Profile ◽  
Wavelength Scanning ◽  
Scanning Interferometer

Thin-film thickness profile measurement using wavelet transform in wavelength-scanning interferometry

2008 ◽  
Vol 46 (2) ◽  
pp. 179-184 ◽  
Author(s):  
Young-Min Hwang ◽  
Sung-Won Yoon ◽  
Jung-Hwan Kim ◽  
Souk Kim ◽  
Heui-Jae Pahk
Keyword(s):  
Thin Film ◽  
Wavelet Transform ◽  
Film Thickness ◽  
Profile Measurement ◽  
Thin Film Thickness ◽  
Thickness Profile ◽  
Wavelength Scanning

Sinusoidal wavelength-scanning interferometer for profile measurement of metal surfaces

2012 ◽  
Author(s):  
Osami Sasaki ◽  
Takahiro Kurashige ◽  
Samuel Choi ◽  
Takamasa Suzuki
Keyword(s):  
Metal Surfaces ◽  
Profile Measurement ◽  
Wavelength Scanning ◽  
Scanning Interferometer

scholarly journals Full-Field Operational Modal Analysis of an Aircraft Composite Panel from the Dynamic Response in Multi-Impact Test

Sensors ◽  
2021 ◽  
Vol 21 (5) ◽  
pp. 1602
Author(s):  
Ángel Molina-Viedma ◽  
Elías López-Alba ◽  
Luis Felipe-Sesé ◽  
Francisco Díaz
Keyword(s):  
Modal Analysis ◽  
Energy Absorption ◽  
High Speed ◽  
Operational Modal Analysis ◽  
Modal Identification ◽  
Image Correlation ◽  
Composite Panel ◽  
Impact Excitation ◽  
Full Field ◽  
The Impact

Experimental characterization and validation of skin components in aircraft entails multiple evaluations (structural, aerodynamic, acoustic, etc.) and expensive campaigns. They require different rigs and equipment to perform the necessary tests. Two of the main dynamic characterizations include the energy absorption under impact forcing and the identification of modal parameters through the vibration response under any broadband excitation, which also includes impacts. This work exploits the response of a stiffened aircraft composite panel submitted to a multi-impact excitation, which is intended for impact and energy absorption analysis. Based on the high stiffness of composite materials, the study worked under the assumption that the global response to the multi-impact excitation is linear with small strains, neglecting the nonlinear behavior produced by local damage generation. Then, modal identification could be performed. The vibration after the impact was measured by high-speed 3D digital image correlation and employed for full-field operational modal analysis. Multiple modes were characterized in a wide spectrum, exploiting the advantages of the full-field noninvasive techniques. These results described a consistent modal behavior of the panel along with good indicators of mode separation given by the auto modal assurance criterion (Auto-MAC). Hence, it illustrates the possibility of performing these dynamic characterizations in a single test, offering additional information while reducing time and investment during the validation of these structures.

scholarly journals Experimental study of the dynamic behaviour of High Performance Concrete (HPC) under tensile loading

2018 ◽  
Vol 183 ◽  
pp. 02043 ◽  
Author(s):  
Bratislav Lukić ◽  
Dominique Saletti ◽  
Pascal Forquin
Keyword(s):  
High Speed ◽  
High Performance ◽  
High Performance Concrete ◽  
Imaging System ◽  
Spall Strength ◽  
High Speed Imaging ◽  
Dynamic Tensile Strength ◽  
Full Field ◽  
Local Point ◽  
Measurement Results

This paper presents the measurement results of the dynamic tensile strength of a High Performance Concrete (HPC) obtained using full-field identification method. An ultra-high speed imaging system and the virtual fields method were used to obtain this information. Furthermore the measurement results were compared with the local point-wise measurement to validate the data pressing. The obtained spall strength was found to be consistently 20% lower than the one obtained when the Novikov formula is used.

Sign in / Sign up

Export Citation Format

Share Document