Lobotomy
发表于 2025-3-23 12:36:58
Göran Goldkuhl,Annie Röstlinger,Ewa Brafloped. Some results of the flutter analysis are presented. The presence of the neighboring blade row gives rise to significant change in the critical flutter fluid velocity for the subsonic cascade when the main acoustic duct mode is of cut-on state.
Grandstand
发表于 2025-3-23 17:57:22
Ewa Brafl the passage shock oscillation. The trailing edge oscillation might be realized by, for instance, application of piezo-electric device. The method was revealed to change the unsteady aerodynamic force acted on the blade from exciting to damping force if the phase of trailing edge oscillation was pr
Missile
发表于 2025-3-23 21:58:42
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MAZE
发表于 2025-3-23 23:24:03
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承认
发表于 2025-3-24 02:45:40
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Fulsome
发表于 2025-3-24 06:43:40
Alexander Mehler,Rodney J. Clarke to historical data, the affect of alternative starting calibration parameters sets on condition number illustrated the limitations of information quality on model uncertainty. Fourth, perfect observed / simulated profiles correlation coefficients for all calibration parameter sets, were, by themsel
改变立场
发表于 2025-3-24 11:36:09
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混合
发表于 2025-3-24 17:49:24
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nonplus
发表于 2025-3-24 21:37:54
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diskitis
发表于 2025-3-25 01:43:15
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