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Vibration-response Tests of a 1/5-scale Model of the Grumman F6F Airplane in the Langley 16-foot High-speed Tunnel
Theodore Theodorsen
Arthur A. Regier
出版
National Advisory Committee for Aeronautics
, 1944
URL
http://books.google.com.hk/books?id=odKdPgAACAAJ&hl=&source=gbs_api
註釋
A series of vibration experiments was conducted in the Langley 16-foot high-speed tunnel on a 1/5-scale model on the Grumman F6F airplane. These tests were conducted to study the vibration responses of the model at airspeeds within the range of the tunnel, or up to approximately 500 miles per hour. Within this range, there was no indication of actual flutter either by shift of frequencies or by decreasing damping. The response curves are given in a series of graphs.
