An investigation of a 1/4-scale supersonic target drone model was performed in the Langley Unitary Plan wind tunnel to determine the effects of various sizes of canards, vertical tails, and ailerons on the aerodynamic characteristics. The tests were made at Mach numbers from 1.57 to 2.10 through an angle-of-attack range from about -5 to 23 deg.
Aerodynamic Characteristics of a Target Drone Vehicle at Mach Numbers from 1.57 to 2.10
1968
72 pages
Report
No indication
English