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Active control of flow through the nozzles at sonic Mach number
by
Ashfaq, Syed
,
Khan, Sher Afghan
,
Rathakrishnan, Ethirajan
Published 2013
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2
Studies on wall pressure flow control by micro jets for high area ratio
by
Ashfaq, Syed
,
Khan, Sher Afghan
Published 2014
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3
Studies on wall pressure of sonic flow through the converging nozzles for different area ratios
by
Ashfaq, Syed
,
Khan, Sher Afghan
Published 2014
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4
Effect of angle of attack on damping derivatives of delta wing with full sine wave curved leading edge
by
Crasta, Asha
,
Khan, Sher Afghan
Published 2015
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RS
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5
Estimation of stability derivatives of a delta wing in hypersonic flow
by
Crasta, Asha
,
Baig, Maugal Ahmed Ali
,
Khan, Sher Afghan
Published 2012
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6
Effect of angle of incidence on roll damping derivatives of a delta wing
by
Crasta, Asha
,
Khan, Sher Afghan
Published 2014
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RS
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