Theoretical stability derivatives for a symmetrically tapered wing of aspect ratio 3 at supersonic speeds- by-A symmetrically tapered wing of aspect ratio 3 and taper ratio FL with streamwise tips describes simple harmonic oscillations of low frequency in supersonic flow....
Tests of round and flat spoilers on a tapered wing in the naca 19-foot pressure wind tunnelSeveral arrangements of round and flat spanwise spoilers attached to the upper surface of a tapered wing were tested in the NACA 19-foot pressure wind tunnel to determine the most effective type, location, and size of spoiler necessary to reduce greatly the lift on the...
The effects of full-span and partial-span split flaps on the aerodynamic characteristics of a tapered wingThe investigation was made to determine the effects of full-span and of partial-span split flaps on the aerodynamic characteristics of a tapered wing....
Measurements and flutter tests model tapered wing oil...Summary.--The influence of various parameters, such as wing density and flexural stiffness on the critical speed of a tapered wing was investigated theoretically in R....
