Sher Afghan Khan

Experimental study on the mean flow characteristics of a supersonic multiple jet configuration

Rakesh Kumar, W. Asrar, M. Faheem, 2021, Aerospace Science and Technology.

Determination of wall pressure flows at supersonic Mach numbers

Abdul Aabid, Sher Afghan Khan, 2020 .

Benefit of Mach number and expansion level on the flow development in a cylindrical tube diameter of 18 mm

Ridwan., M. Faheem, Sher Afghan Khan, 2021 .

Impact of expansion level on flowfield with sudden expansion at supersonic regimes

Ridwan., M. Faheem, Sher Afghan Khan, 2021 .

Effect of expansion level on the flow development with sudden expansion at high Mach numbers

Ridwan., M. Faheem, Sher Afghan Khan, 2021 .

Numerical Analysis of Cavity-Based Control of Base Pressure Variations at Supersonic Mach Numbers

Abdul Aabid, Sher Afghan Khan, Ridwan, 2023, Fluid Dynamics & Materials Processing.

Passive Control of Base Pressure in a Converging-Diverging Nozzle with Area Ratio 2.56 at Mach 1.8

Abdul Aabid, M. Baig, Sher Afghan Khan, 2023, Fluid Dynamics & Materials Processing.