An adaptive integration surface for predicting transonic rotor noise in hovering and forward flights
.org/10.1016/j.cja.2019.04.006 1000-9361?2019 Production and hosting by Elsevier Ltd. on behalf of Chinese Society of Aeronautics and Astronautics. This is an open access article under the CC BY-NC-ND license (http://creativecommons.org/licenses/by-nc-nd/4.0/).
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2019-11-08(万方平台首次上网日期,不代表论文的发表时间)
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2047-2058