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Suggestions 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
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