Longitudinal frequency-response characteristics of a 35 degree swept-wing airplane as determined from flight measurements, including a method for the evaluation of transfer functions

William C. Triplett, G. Allan Smith
naca-rm-a51g27
Sep 1951


Longitudinal frequency-response characteristics of a 35 degree swept-wing airplane computed from flight measurements are presented. Pitching-velocity and normal acceleration responses to pulse-type elevator inputs have been analyzed to obtain frequency responses and numerical values of the coefficients of the transfer functions.

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