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Mathematical model of acoustic flutter of supersonic grills

โœ Scribed by A. V. Gubarev; S. A. Laptev


Publisher
SP MAIK Nauka/Interperiodica
Year
1992
Tongue
English
Weight
312 KB
Volume
33
Category
Article
ISSN
0021-8944

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Aero-thermoelastic analysis of a simply supported functionally graded truncated conical shell subjected to supersonic air flow is performed to predict the flutter boundaries. The temperature-dependent properties of the FG shell are assumed to be graded through the thickness according to a simple rul