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Vibration Surveys of the P-40 Rudder and Fin-rudder Assembly
註釋Included are surveys on the vibration response of the P-40 rudder and fin-rudder assembly were conducted during the fall of 1942 for the purpose of obtaining information on the flutter characteristics of high-speed airplanes of known performance. This work is a continuation of similar study on the P-47 airplane. The tests on the rudder alone were made with the rudder suspend in the floating condition; the tests on the fin-rudder unit were made with the fin rigidly fasted to a concrete base. In the figures the plus and minus signs are used to signify opposite phases with the size of each sign proportional to the amplitude. In several figures the nodal lines are drawn.