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70 积分 2026-01-08 加入
“An Experimental Investigation at a Mach Number of 2.01 of the Effects of BodyCross-Section Shape on the Aerodynamic Characteristics of Bodies and Wing-Body Combinations
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Experimental Investigation of the Low-Speed Aerodynamic Characteristics of a 5.8-Percent Scale Hybrid Wing Body Configuration
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Computational aerodynamic investigation of long strake-tail missile config
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Aerodynamics of an Axisymmetric Missile Concept Having Cruciform Strakes and In-Line Tail Fins From Mach 0.60 to 4.63
6个月前
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High Angle of Attack Aerodynamic Predictions Using Missile Datcom
6个月前
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Experimental and numerical comparison of different missile body cross sectional shapes
6个月前
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