absolve 发表于 2025-3-25 05:20:30
7楼偏狂症 发表于 2025-3-25 10:50:05
7楼遗留之物 发表于 2025-3-25 13:43:29
7楼凹处 发表于 2025-3-25 18:21:24
7楼photopsia 发表于 2025-3-25 23:41:04
8楼Exuberance 发表于 2025-3-26 00:35:29
8楼inveigh 发表于 2025-3-26 06:59:45
8楼Polydipsia 发表于 2025-3-26 10:22:24
8楼灾祸 发表于 2025-3-26 13:40:46
http://reply.papertrans.cn/77/7626/762531/762531_29.pngSuggestions 发表于 2025-3-26 20:27:23
Quantenmechanik für Fortgeschrittene (QM II) method is applied to compute the pressure fluctuations due to jet noise on the outer skin of the fuselage. For the turbulent boundary layer, analytic calculations of auto-spectra and wavenumber-spectra are transferred to pressure fluctuations on the outer skin as well. The loads are applied to a wa