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Single-degree-of-freedom-flutter Calculations for a Wing in Subsonic Potential Flow and Comparison with an Experiment
Harry L. Runyan
出版
National Advisory Committee for Aeronautics
, 1951
URL
http://books.google.com.hk/books?id=-Sd5l1F81scC&hl=&source=gbs_api
EBook
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註釋
The effect of Mach number and structural damping on single-degree-of-freedom pitching of a wing is presented in this report. Some experimental results are compared with theory and good agreement is found for certain ranges of an inertia parameter.