intention
发表于 2025-3-28 15:30:58
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FLEET
发表于 2025-3-28 18:45:39
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Demonstrate
发表于 2025-3-29 01:45:43
The Matter of Discrete Euler Solutions for Lifting Wings,With the development in particular of fighter aircraft with delta-type wings the phenomenon of lee-side vortices became a topic in the field of aerodynamics.
NORM
发表于 2025-3-29 06:57:11
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BAN
发表于 2025-3-29 10:36:19
Small Aspect-Ratio Delta-Type Wing Flow,Studied in this chapter are the lee-side vortex systems of small aspect-ratio delta-type wings, which lead to the phenomenon of non-linear lift. Small aspect-ratio delta-type wings encompass delta wings, usually in combination with a canard and hybrid wings, i.e., trapezoidal wings in combination with strakes.
AMEND
发表于 2025-3-29 11:55:33
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反叛者
发表于 2025-3-29 17:06:11
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安慰
发表于 2025-3-29 22:01:12
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游行
发表于 2025-3-30 02:29:58
The Local Vorticity Content of a Shear Layer,ign work. At that time very much discussed was the fact that at delta wings with sharp leading edges lee-side vortices resulted in the relevant angle of attack and Mach number regime. The question was, where is the apparent vorticity coming from, and accordingly the associated entropy rise.
Hemiplegia
发表于 2025-3-30 07:40:39
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