Wind tunnel tests of a 0.04 scale model of Avro C-105 vertical tail at supersonic speeds
Entry/Object ID
3428
Category
Report - Technical
Archive Items Details
Description
Tests have been made in the N.A.E. 30" x 16" high speed wind tunnel on a 0.04 scale model of the vertical tail of the C-105 aircraft to determine the vertical tail load characteristics and rudder hinge moment data. The tests were made at Mach numbers 1.22, 1.35, 1.57, 1.78 and 2.03. The corresponding Reynolds number range is shown in figure 4.
