Loads measured on the horizontal tail, vertical tail, and wing and the aeroelastic distortions of elevators, stabilizers, and fuselage of a B-45A airplane in a right and left roll at a Mach number of 0.60 and an altitude of 15,000 feet are presented. The data are given in time-history form.
Time Histories of Loads and Deformation on a B-45A Airplane in Two Aileron Rolls
1949
25 pages
Report
No indication
English