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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	FULL_PUBLIC_DOMAIN

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.