A method is given for determining the horizontal tail loads in maneuvering flight. The method is based upon the assignment of a load-factor variation with time and the determination of a minimum time to reach peak load factor. The tail load is separated into various components. Examination of these components indicated that one of the components was so small that it could be neglected for most conventional airplanes, thereby reducing to a minimum number of aerodynamic parameters needed in this computation of tail loads.
Horizontal Tail Loads in Maneuvering Flight
1950
33 pages
Report
Keine Angabe
Englisch
Horizontal tail loads in maneuvering flight
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