激怒某人
发表于 2025-3-26 23:51:04
978-981-16-6642-1The Editor(s) (if applicable) and The Author(s), under exclusive license to Springer Nature Singapor
等待
发表于 2025-3-27 01:42:12
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Fulsome
发表于 2025-3-27 05:54:03
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商品
发表于 2025-3-27 10:51:50
Numerical Study on Aerodynamic Performance of Hypersonic Vehicle with Aerospikess on the aerospike’s . ratios. Among the different aerospike configurations studied, the drag reduction effect of aerospike when the . = 1 is the best, and the maximum value of the drag reduction efficiency is 36.4%. Within the scope of this study, as the . ratio of the aerospike increases, the drag
NAUT
发表于 2025-3-27 16:50:39
Terminal Multi-Constrained Finite Time Sliding Mode Guidance Law Based on Truncation Function for Hyees of freedom in the transverse plane to ensure the constraint of impact velocity. The simulation verified that the guidance method can meet the requirements of terminal multiple constraints of hypersonic vehicle.
cunning
发表于 2025-3-27 20:02:19
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hyperuricemia
发表于 2025-3-27 23:50:41
Dynamic Detection Method for Blade Tip Clearance of Aero-Engine in Assembled State Based on Linear Sa. Compared to the traditional methods, the BTC in whole circumferential phase can be measured rather than single phase. Meanwhile, the proposed method is not influenced by casing deformation and installation errors. Finally, the feasibility and capability of the system is verified by simulation exp
有恶意
发表于 2025-3-28 03:39:23
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过分自信
发表于 2025-3-28 10:15:10
Design and Optimization of the Flexible Support Structure for Space Mirrorflexure hinges were established aiming at maintaining high static precision of the mirror under multi-conditions, and the resilient connector was optimized by stress deconcentration and viscoelastic materials damping to obtain adequate dynamic strength margin. Finally, the comprehensive performance
阴谋小团体
发表于 2025-3-28 11:47:44
Target Localization on Image-Guided Missilecoordinate system. The proposed method is validated in the flight data of a certain type of image-guided missile, and a high-precision localization result is obtained at a long missile-target distance.