Hinge-moment, lift, and pitching-moment characteristics of a flap-type control surface having various hinge-line locations on a 4-percent-thick 60 degree delta wing: transonic bump method
Description: Report presenting an investigation in the high-speed tunnel to determine the hinge-moment, lift, and pitching-moment characteristics of a 4-percent-thick 60 degree delta wing with a trailing-edge flap-type control. The purpose of this investigation is to determine the ideal aerodynamic balance of a large part of the control force in order to make aircraft easier to control in the event of power failure.
Date: March 24, 1954
Creator: Thompson, Robert F.
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