Flutter calculations were based on modified strip-analysis method of N ACA Research Memo L57L10 and covered Mach numbers from 0 to 1.75; flutter suppressor consists of small mass connected to wing by means of flexible sting; 3 suppressor masses were investigated but no attempt was made to make configuration optimum.
Theoretical investigation of subsonic and supersonic flutter characteristics of swept wing employing tuned sting-mass flutter suppressor
NASA -- Tech Note
1960
45 pages
Article (Journal)
English
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