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    Browsing by Advisor "Venkatakrishan, L"

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      • Control of shock-induced vortex breakdown in Transonic regime on a slender delta wing body configuration using blowing 

        Kurade, Rajan Bharat
        Modern high speed aircrafts feature highly swept and low aspect ratio wings, mainly to increase the critical Mach number and reduce the wave drag. A special case of swept wings is wings with triangular planform commonly ...

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