Description
Tests have been made in the NAE 30" x 16" high speed wind tunnel on a .04 scale model of the vertical tail of the Avro Arrow aircraft to determine the effect of the I.R. seeker pod on the vertical tail characteristics and on rudder hinge moments. The tests were made at Mach numbers 1.35, 1.78 and 2.03. The corresponding Reynolds number range was between 2.36 and 1.98 x 10?.