An investigation has been conducted in the Langley Unitary Plan wind tunnel to determine the aerodynamic characteristics of a revised target drone vehicle through a Mach number range from 1.60 to 2.86. The vehicle had canard surfaces and a swept clipped-delta wing with twin tip-mounted vertical tails.
Aerodynamic Characteristics of a Revised Target Drone Vehicle at Mach Numbers from 1.60 to 2.86
1968
54 pages
Report
Keine Angabe
Englisch
Aerodynamics , Aircraft , Aerodynamic characteristics , Delta wings , Canard configurations , Drone vehicles , Swept wings , Wind tunnel tests , Supersonic speed , Wind tunnel models , Aerodynamic stability , Stabilizers(Fluid dynamics) , Mach number , Tail assemblies , Angle of attack , Longitudinal stability