A novel type of high-speed swirl nozzle was biomimetically designed based on the wing profile of a frigatebird and streamlined. The wing profile of the frigatebird with scimitar-shaped protrusions is adopted as the side wall of the swirl tube. The spiral direction of the swirl tube is designed such that the protrusion side faces forward to break through the gas flow. The superior gas stability and gas-liquid mass transfer capability resulting from this biomimetic design was confirmed through a combination of experiments and numerical simulation. Due to the gas dispersion effect of the swirl holes, high-frequency unstable oscillations in the initial section of the jet are alleviated. The coalescence of microbubbles is weakened, resulting in the reduction of the jet expansion amplitude. The corresponding gas reverse impact is weakened. The superior stability can be quantitatively analyzed. Variance and Allan deviation of the jet root radius is half that of a pressure-type nozzle. The high-frequency signals of the jet root radius in the range of 100-150 Hz have been significantly reduced as determined by the Continuous Wavelet Transform. Besides, the jet half-width of the novel nozzle is 3.16 times that of a straight-tube and 1.89 times that of a pressure-type nozzle. Due to the acceleration effect, the horizontal penetration depth of the novel swirl nozzle is 2.15 to 2.37 times that of a straight-tube, and reaches 52.93 % to 73.09 % of that of a pressure-type nozzle. Numerical simulation determined that flow field velocity under the novel swirl nozzle can be improved in the double-side-blown process. The gas-liquid mass transfer capability is 1.66 times that of the straight-tube. The component diffusion capability is 1.49 times that of the straight-tube.
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