Supervised by: China Aerospace Science and Technology Corporation
Sponsored by: China Academy of Aerospace Aerodynamics
Chinese Society of Astronautics
China Aerospace Publishing House Co., LTD
ZHAO Rui, ZHANG Xin-xin, WEN Chihyung, et al. Investigation and Optimization of Acoustic Metasurfaces to Depress Mack Second Mode in Hypersonic Boundary-Layer Flow[J]. PHYSICS OF GASES, 2018, 3(6): 35-40. DOI: 10.19527/j.cnki.2096-1642.2018.06.005
Citation: ZHAO Rui, ZHANG Xin-xin, WEN Chihyung, et al. Investigation and Optimization of Acoustic Metasurfaces to Depress Mack Second Mode in Hypersonic Boundary-Layer Flow[J]. PHYSICS OF GASES, 2018, 3(6): 35-40. DOI: 10.19527/j.cnki.2096-1642.2018.06.005

Investigation and Optimization of Acoustic Metasurfaces to Depress Mack Second Mode in Hypersonic Boundary-Layer Flow

  • A theoretical model to describe the acoustic characteristics of plane ultrasonic acoustic waves imping on an acoustic metasurface was developed. The proposed model takes into account the high-order diffracted modes and therefore incorporates mutual coupling among neighboring cavities. With this model, the cavity geometry parameters were optimized to achieve the minimum reflection coefficient and impedance, respectively. Results reveal that the phase opposition between incident and reflective waves at the surface could largely depress the increment ratio of Mack second mode. The proposed effective impedance boundary could open up new possibilities of metasurfaces for hypersonic boundary-layer transition control.
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