Journal papers
[1] Zhou, D., Wang, K. & Wang, M., Space-Time characteristics of wall-pressure fluctuations beneath an axisymmetric turbulent boundary layer with adverse pressure gradient. (In preparation)
[2] Zhou, D., Wang, K. & Wang, M., Evolution of a non-equilibrium turbulent boundary layer on the tail cone of a body of revolution under strong adverse pressure gradient. (In preparation)
[3] Zhou, D., Wang, X., Jing, X. & Sun, X., Acoustic properties of multiple cavity resonance liner for absorbing higher-order duct modes. The Journal of the Acoustical Society of America, 140 (2016), pp. 1251–1267.
[4] Zhou, D., Wang, X., Chen, J., Jing, X. & Sun, X., Sound generation by non-synchronously oscillating rotor blades in turbomachinery. Journal of Sound and Vibration, 355 (2015), pp. 150–171.
[5] Zhou, D., Wang, X., Chen, J., Jing, X. & Sun, X., Investigation of sound generation by nonsynchronously viberating rotor blades. Acta Aeronautica et Astronautica Sinica, 36 (2015), pp. 737–748.
Conference papers
[1] Zhou, D., Wang, K. & Wang, M., Computation of rotor noise generation in a thick axisymmetric turbulent boundary layer. AIAA AVIATION 2021 FORUM, Aug. 2021 (accepted).
[2] Zhou, D., Wang, K. & Wang, M., Large-Eddy simulation of an axisymmetric boundary layer on a body of revolution, AIAA 2020-2989. AIAA AVIATION 2020 FORUM, June 2020.
[3] Zhou, D., Wang, X. & Sun, X., Investigation on the broadband noise absorption performance of multiple cavity resonance liner. The 22nd International Congress on Sound and Vibration, July 2015.
[4] Wang, X., Zhou, D. & Sun, X., Investigation on effect of rotor blades on the sound propagation. The 22nd International Congress on Sound and Vibration, July 2015.
[5] Zeng, Z., Zhou, D. & Wang, X., Experimental research on the upstream propagating rotor-stator interaction noise of axial compressor. Western China Symposium for Acoustic Technology 2015, July 2015.