Simultaneous determination of thermal conductivities of thin film and substrate by extending 3ω-method to wide-frequency range

2007 ◽  
Vol 253 (22) ◽  
pp. 9024-9029 ◽  
Author(s):  
Zhao Liang Wang ◽  
Da Wei Tang ◽  
Xing Hua Zheng
Keyword(s):  
Thin Film ◽  
Simultaneous Determination ◽  
Wide Frequency Range ◽  
Frequency Range ◽  
3Ω Method ◽  
Thermal Conductivities

A highly selective and simultaneous determination of ascorbic acid, uric acid and nitrite based on a novel poly-N-acetyl-l-methionine (poly-NALM) thin film

RSC Advances ◽  
2016 ◽  
Vol 6 (99) ◽  
pp. 96898-96907 ◽  
Author(s):  
Ayyadurai Kannan ◽  
Arumugam Sivanesan ◽  
Govindasamy Kalaivani ◽  
Arumugam Manivel ◽  
Ranganathan Sevvel
Keyword(s):  
Thin Film ◽  
Ascorbic Acid ◽  
Uric Acid ◽  
Polymer Film ◽  
Simultaneous Determination ◽  
Glassy Carbon Electrode ◽  
Glassy Carbon ◽  
Carbon Electrode ◽  
Facile Fabrication

This paper demonstrates the facile fabrication of an N-acetyl-l-methionine (NALM) polymer film on a glassy carbon electrode (GCE) by an electropolymerization technique.

A New Method for Simultaneous Determination of Anisotropic Thermal Conductivities Based on Two-Dimensional Analysis

2001 ◽  
Vol 40 (Part 1, No. 1) ◽  
pp. 388-392
Author(s):  
Hiroyuki Fujishiro ◽  
Tatsuya Okamoto ◽  
Manabu Ikebe ◽  
Koichi Hirose
Keyword(s):  
Simultaneous Determination ◽  
Dimensional Analysis ◽  
New Method ◽  
Two Dimensional ◽  
Thermal Conductivities

Prediction of Turbomachinery Aeroelastic Behavior From a Set of Representative Modes

2011 ◽  
Author(s):  
Mari´a A. Mayorca ◽  
Damian M. Vogt ◽  
Hans Ma˚rtensson ◽  
Torsten H. Fransson
Keyword(s):  
Wide Frequency Range ◽  
Least Square ◽  
Mode Shapes ◽  
Frequency Range ◽  
Reduced Order ◽  
Transonic Compressor ◽  
Unsteady Aerodynamic ◽  
Shape Perturbation ◽  
Selection Of

A method is proposed for the determination of the aeroelastic behavior of a system responding to mode-shapes different to the tuned in-vacuo ones, due to mistuning, mode family interaction or any other source of mode-shape perturbation. The method is based on the generation of a data base of unsteady aerodynamic forces arising from the motion of arbitrary modes and uses Least Square approximations for the prediction of any responding mode. The use of a reduced order technique allows for mistuning analyses and is also applied for the selection of a limited number of arbitrary modes. The application on a transonic compressor blade shows that the method captures well the aeroelastic properties in a wide frequency range. A discussion of the influence of the mode-shapes and frequency on the final stability response is also provided.

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