Delta Wing Study Shows Suction Peak Does Not Sit Under the Vortex Center
Combined pressure-sensitive paint and particle image velocimetry measurements on a 70-degree slender delta wing show that the suction peak does ...
Combined pressure-sensitive paint and particle image velocimetry measurements on a 70-degree slender delta wing show that the suction peak does ...
A cable-driven parallel suspension system has enabled wind tunnel tests of unstable, variable-frequency and variable-amplitude maneuvers, revealing complex aerodynamic hysteresis ...
Combined wind tunnel tests and simulations at Mach 6 show an opposing jet cuts blunt-body drag by up to 32.67 ...
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