Sentence examples for specimens was evaluated using from inspiring English sources
Effect of UV exposure on color change of composite specimens was evaluated using colorimetry.
Hence, the wear of all the specimens was evaluated using the pin-on-disc test, with a high-speed steel disc.
The corrosion resistance of the Ni–W alloy coated specimens was evaluated using potentiodynamic polarization (Tafel) and electrochemical impedance spectroscopy (EIS) studies.
The linear firing shrinkage values were determined according to the formula given in the standard ANSI/ADA (American National Standards Institute/American Dental Association) 69 and the flexural strength of the specimens was evaluated using 3-point bending test.
The effect of elevated temperature on bond strength using concrete/polymer adhesive/FRP specimens was evaluated using four different test methods namely; slant shear test as per BS 6319 Part 4, tensile bond strength test as per ASTM C952, shear bond strength test as per ASTM D905 and double-face shear bond strength.
The morphology of other specimens was evaluated using descriptions and illustrations provided in original publications.
The effect of nanoclay on the chemical composition and microstructure of heat-damaged specimens were evaluated using XRD and SEM tests, respectively.
Hardness and elastic modulus of the specimens were evaluated using both the continuous stiffness measurement (CSM) and the unloading stiffness measurement (USM) method.
The specimens were evaluated using cyclic oxidation tests and important properties of the TBCs, such as resistance to sintering and phase transformation, were determined.
In this article, key design parameters including Unconfined Compressive Strength (UCS), resilient moduli (MR) and permanent deformation characteristics of CG-geopolymer remoulded cylindrical specimens are evaluated using simulated long-term Repeated Load Triaxial (RLT) tests.
In previous work, results from experiments on Ti 6Al 4V pads and specimens were evaluated using finite element analyses where stress intensity factors were calculated assuming a single-edge tension, Mode I crack to form.
