Low Reynolds Number Wind Tunnel - V., Somashekar
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In the future, wind tunnel may be required to achieve multiple mission objectives in a single platform. To enable this capability the concept of 360 degree rotatable test section wind tunnel variable geometry has been proposed as a means to extend the capability of current Low Reynolds number air vehicle platforms. This requires the development of seamless structure/aerodynamic structures that can undergo large scale changes in low Reynolds number wind tunnel geometry. The above discussion on wind tunnel has generated lot of interest in wind tunnel weight, geometry, complexity, structure, and aerodynamic performance etc.…mehr

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Produktbeschreibung
In the future, wind tunnel may be required to achieve multiple mission objectives in a single platform. To enable this capability the concept of 360 degree rotatable test section wind tunnel variable geometry has been proposed as a means to extend the capability of current Low Reynolds number air vehicle platforms. This requires the development of seamless structure/aerodynamic structures that can undergo large scale changes in low Reynolds number wind tunnel geometry. The above discussion on wind tunnel has generated lot of interest in wind tunnel weight, geometry, complexity, structure, and aerodynamic performance etc.
Autorenporträt
Mr SOMASHEKAR V, a well-known Assistant Professor and Researcher. He has a mixed experience of industry as well as teaching in the area of Aeronautical and Mechanical Engineering. He has published several research papers and books in international Publications. His area of research includes: Aerodynamics, Experimental Aerodynamics, Wind Tunnel etc.