Liquid Crystal Thermography for Gas Turbine Heat Transfer Measurements
A special issue of Crystals (ISSN 2073-4352). This special issue belongs to the section "Liquid Crystals".
Deadline for manuscript submissions: closed (30 April 2021) | Viewed by 8538
Special Issue Editors
Interests: liquid crystal thermography; infrared thermography; porous media heat transfer; phase change materials; carbonaceous materials; additive manufacturing
Special Issue Information
Dear Colleagues,
With the ever-increasing push for achieving higher turbine inlet temperatures in gas turbines, the hot gas path components, such as nozzle guide vanes, 1st-stage stator vanes and rotor blades, their endwalls, are subjected to extremely harsh environments with gas temperatures in excess of 1500 °C. To protect these components, relatively coder air bled off from the compressor section is routed to the internal cooling passages of vanes and blades and eventually allowed to escape into the hot gas path via film cooling holes. The fundamental objective of cooling designers is to enhance the convective heat transfer coefficient between internally routed air and airfoil internals, and enhanced film cooling effectiveness and its coverage of the airfoil outer skin, with resourceful coolant usage. This task requires dedicated studies on the development of advanced heat exchangers with complex flow paths. Liquid crystal thermography enables the determination of local surface temperature through image processing of the color change when the surface temperature on which the encapsulated thermochromic liquid crystals (TLC) are sprayed upon reaches a certain temperature. This information is then used for the determination of local convective heat transfer coefficients and adiabatic film cooling effectiveness through direct or inverse heat transfer techniques.
This topic invites papers focused on the broad areas of gas turbine heat transfer where liquid crystal thermography is employed under both stationary and rotating operating conditions for detailed measurements of heat transfer quantities. Papers focused on image processing, image noise reduction, color perception, calibration methods, advanced instrumentations for image acquisition, TLC surface illumination, TLC surface preparation methods, TLC spray coating effects, TLC degradation, etc. are also invited. Papers are also sought which employ advanced solid heat diffusion modeling techniques using detailed surface temperature data through liquid crystals for the determination of the above heat transfer quantities.
Dr. Prashant Singh
Prof. Dr. Lesley Wright
Guest Editors
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Keywords
- Liquid crystal thermography
- Gas turbines
- Heat transfer
- Film cooling performance
- Inverse heat transfer
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