带来墨水
发表于 2025-3-26 22:18:46
Investigation on Turbulence Structures in the Wake of a Generic Rocket Configuration,copic Particle Image Velocimetry (PIV) provided statistical turbulence information on the unsteady wake flow with high spatial resolution. Multiple perpendicular regions of interest (ROI) were combined to generate three-dimensional views. Distinct flow patterns emerged that can be interpreted as a r
壕沟
发表于 2025-3-27 04:58:00
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Fatten
发表于 2025-3-27 08:50:30
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Misgiving
发表于 2025-3-27 13:22:36
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错
发表于 2025-3-27 13:39:28
Wind Tunnel and Flight Tests with Active Flow Control on a S10 Glider Configuration,nel and flight tests. A periodic pulsating jet, coupled in from the suction side of the flap near the separation area, was used to delay flow separation for both cases. The wind tunnel experiments were carried out in a closed loop wind tunnel at a Reynolds number of .. = 1.75·10.. In addition to mea
收藏品
发表于 2025-3-27 19:20:47
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GLADE
发表于 2025-3-27 23:51:20
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fluffy
发表于 2025-3-28 04:34:26
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一致性
发表于 2025-3-28 09:08:31
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CAND
发表于 2025-3-28 10:37:45
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