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Supersonic flutter analysis of wings using an unsteady 3D panel method

โœ Scribed by Jinsoo Cho; Younhyuck Chang

Book ID
108391154
Publisher
Elsevier Science
Year
2001
Tongue
English
Weight
494 KB
Volume
30
Category
Article
ISSN
0045-7930

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๐Ÿ“œ SIMILAR VOLUMES

Steady/unsteady aerodynamic analysis of
Steady/unsteady aerodynamic analysis of wings at subsonic, sonic and supersonic Mach numbers using a 3D panel method
โœ Jeonghyun Cho; Cheolheui Han; Leesang Cho; Jinsoo Cho ๐Ÿ“‚ Article ๐Ÿ“… 2003 ๐Ÿ› John Wiley and Sons ๐ŸŒ English โš– 156 KB

## Abstract This paper treats the kernel function of an integral equation that relates a known or prescribed upwash distribution to an unknown lift distribution for a finite wing. The pressure kernel functions of the singular integral equation are summarized for all speed range in the Laplace trans