Zobrazeno 1 - 10
of 119
pro vyhledávání: '"Serhiy Yarusevych"'
Publikováno v:
Physics of Fluids. 35
Aerodynamics of finite-span inclined square flat plates is experimentally investigated at a chord-based Reynolds number of 50 000 in ground effect. The minimum ground height is varied between gap ratios of 0.1 to 1.0 in chord lengths. All components
Autor:
Connor Toppings, Serhiy Yarusevych
Publikováno v:
Experiments in Fluids. 64
Publikováno v:
Experiments in Fluids: experimental methods and their applications to fluid flow, 64(4)
This investigation explores the utility of Alternating Current, Dielectric Barrier Discharge (AC-DBD) plasma actuators for producing three-dimensional disturbances of a desired spanwise wavelength via superposition. The technique utilizes two pairs o
Externí odkaz:
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http://resolver.tudelft.nl/uuid:a2c2cf78-ec8c-49d9-880f-97f2c913526d
Autor:
Yash Shah, Serhiy Yarusevych
Publikováno v:
Physical Review Fluids. 7
Autor:
Connor Toppings, Serhiy Yarusevych
Publikováno v:
International Journal of Heat and Fluid Flow. 101:109141
Autor:
Connor E. Toppings, Serhiy Yarusevych
Publikováno v:
Journal of Fluid Mechanics. 944
The influence of the wing root junction on the laminar separation bubble forming on the suction surface of a semispan NACA 0018 wing cantilevered from the wind tunnel test section wall is studied using surface flow visualisations, particle image velo
Publikováno v:
AIAA Journal. :1-13
This experimental study considers the development of a laminar separation bubble formed over a finite wing and contrasts it with the flow evolution over a two-dimensional airfoil. The experiments w...
Publikováno v:
AIAA Journal. 59:493-505
Three-dimensional flow development is experimentally assessed in a convectively unstable laminar separation bubble formed over a NACA 0018 airfoil at a chord Reynolds number of 125,000, an angle of...
Autor:
Connor E. Toppings, Serhiy Yarusevych
Publikováno v:
Journal of Fluid Mechanics. 929
The three-dimensional flow topology of a laminar separation bubble forming on the suction surface of a semispan wing with an aspect ratio of $2.5$ and NACA 0018 airfoil section is characterised experimentally using surface pressure measurements and p