Longitudinal and Lateral Stability and Control Characteristics of a 1/9-Scale Model of a Twin-Ramjet Canard Target Drone at Mach Numbers from 0.60 to 2.80

摘要

Tests were made in the Langley 8-foot transonic pressure tunnel at Mach numbers from 0.60 to 1.20 and in the Langley Unitary Plan tunnel at Mach numbers of 1.60, 1.80, 2.16, and 2.80. Tests were made at combined angles of attack and sideslip with various combinations of control deflections for the model both with and without boosters.