Although plenty of techniques are employed to improve cooling performance of turbine blades, the improvement was mainly achieved by enhancing convective heat transfer, while radiative heat transfer was not utilized. Besides, most of the existing investigations on the cooling channel were conducted under low thermal load conditions. To bridge these research gaps, this study presents a novel experimental investigation of the convective-radiative synergistic heat transfer enhancement in cooling channels with radiation enhancement plate. The experiments under high thermal load conditions up to 25,000 W m−2 are carried out. Two kinds of novel channel configurations are developed with smooth or ribbed radiation enhancement plate, which can expand cold surfaces to strengthen radiation. The research indicates that, comparing with the traditional channel configuration, growths of total Nusselt number ratio as well as comprehensive thermal performance are 69.70 % and 24.62 %, respectively, by employing the smooth radiation enhancement plate. When inclined ribs are arranged on the radiation enhancement plate, growths of total Nusselt number ratio as well as comprehensive thermal performance are 82.58 % and 9.23 %, respectively, because airflow disturbance in the core region is intensified. The total Nusselt number ratio drops as Reynolds number grows, while it increases as wall heat flux rises. Besides, the approximate analysis method and the fitting method are developed to predict the channel wall temperature and the cooling performance, which is beneficial to overcome the limitation of equipment and experimental conditions for high thermal loads. In addition, the decoupling of convective and radiative heat transfer is achieved. Influences of radiative heat transfer on the overall thermal performance are also quantitatively explored.


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