Author Search Results

1

Influence of low length-to-diameter ratio and nozzle pressure ratio in an abruptly expanded flow

by Khan, Sher Afghan
Published 2015

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2

Active control of suddenly expanded flows from overexpanded nozzles

by Khan, Sher, Rathakrishnan, E.
Published 2002

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3

Investigation of efficacy of low length-to-diameter ratio and nozzle pressure ratio on base pressure in an abruptly expanded flow

by Ahmed, Fharrukh, Khan, Sher Afghan
Published 2018

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4

Optimization of heat transfer on thermal barrier coated gas turbine blade

by Aabid, Abdul, Khan, Sher Afghan
Published 2018

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5

Design and fabrication of flying saucer utilizing coanda effect

by Aabid, Abdul, Khan, Sher Afghan
Published 2018

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6

Base pressure control using micro-jets in supersonic flow regimes

by Sethuraman, Vigneshvaran, Khan, Sher Afghan
Published 2018

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7

Active control of suddenly expanded flow from under expanded nozzles

by Khan, Sher Afghan, Rathakrishnan, E.
Published 2004

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8

Effect of aspect ratio with angle of attack of an oscillating hypersonic delta wing with straight leading edges

by Crasta, Asha, Khan, Sher Afghan
Published 2015

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9

Active control of suddenly expanded flow

by Khan, Sher Afghan, Sellappan, Rathakrishnan
Published 2000

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10

Control of suddenly expanded flows with micro-jets

by Khan, Sher Afghan, Rathakrishnan, E.
Published 2003

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11

Control of suddenly expanded flow from correctly expanded nozzles

by Khan, Sher Afghan, Rathakrishnan, E.
Published 2004

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12

Nozzle expansion level effect on a suddenly expanded flow

by Khan, Sher Afghan, Rathakrishnan, E.
Published 2006

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13

Control of base pressure with micro jets:part-I

by Rehman, Shafiqur, Khan, Sher Afghan
Published 2008

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14

Active control of base pressure in supersonic regime

by Khan, Sher Afghan, Rathakrishnan, E.
Published 2006

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15

Control of suddenly expanded flow

by Khan, Sher Afghan, Rathakrishnan, E.
Published 2006

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16

Oscillating supersonic delta wings with curved leading edges

by Khan, Sher Afghan, Crasta , Asha
Published 2010

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17

High incidence supersonic similitude for planar wedge

by Crasta, Asha, Khan, Sher Afghan
Published 2012

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18

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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19

Estimation of stability derivatives of an oscillating hypersonic delta wings with curved leading edges

by Crasta, Asha, Khan, Sher Afghan
Published 2012

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20

Stabilty derivatives in the newtonian limit

by Crasta, Asha, Khan, Sher Afghan
Published 2013

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Sher Khan