๐”– Bobbio Scriptorium
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Separated supersonic flow past a trailing edge at incidence

โœ Scribed by J.W. Elliott; F.T. Smith


Publisher
Elsevier Science
Year
1986
Tongue
English
Weight
560 KB
Volume
14
Category
Article
ISSN
0045-7930

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๐Ÿ“œ SIMILAR VOLUMES


TRAILING EDGE NOISE AT LOW MACH NUMBERS,
โœ M.S. HOWE ๐Ÿ“‚ Article ๐Ÿ“… 2000 ๐Ÿ› Elsevier Science ๐ŸŒ English โš– 314 KB

The di!raction theory of Part 1 [1] for estimating the sound generated by low Mach number #ow past the trailing edge of an airfoil of compact, but "nite thickness is applied to investigate the noise produced by turbulent #ow over an edge whose upper surface pro"le (the suction side) is rounded. The