activity
20202026
most citedUnsteadiness in hypersonic leading-edge separation

10 citations · 23 across the 5 of their papers we have counts for

collaborators

5 papers

physics.flu-dyn2026

Axisymmetric cavities in hypersonic flow

Soumya R. Nanda, T. V. Krishna, S. K. Karthick +1

A detailed experimental campaign is conducted to investigate the shear layer characteristics of an axisymmetric open cavity exposed to a Mach freestream. Experiments are perfor…

physics.flu-dyn2022★ 10 cited

Unsteadiness in hypersonic leading-edge separation

S. K. Karthick, Soumya R. Nanda, J. Cohen

Hypersonic leading-edge separation is studied towards understanding the varying shock-related unsteadiness with freestream Reynolds number ($1.66 \times 10^5 \leq Re_D \leq 5.85 \t…

physics.flu-dyn2021★ 7 cited

On Spherical Shock Wave focusing in Air -- a Computational Study

Saranyamol V. S., Soumya Ranjan Nanda, Mohammed Ibrahim S

A detailed numerical study on the phenomenon of Shock Wave focusing in air is carried out. The focusing phenomenon is achieved with the help of a shock tube and a converging sectio…

physics.flu-dyn2021★ 6 cited

On the unsteady dynamics of partially shrouded compressible jets

Soumya R. Nanda, S. K. Karthick, T. V. Krishna +2

We experimentally investigate a partially shrouded sonic jet (a sonic free-jet shielded by a solid wall-extension on one side) exiting from a planar nozzle at two different nozzle…

physics.flu-dyn2020

On the fluidic behavior of an over-expanded planar plug nozzle under lateral confinement

M. Chaudhary, T. V. Krishna, Sowmya R. Nanda +4

The present work aims to study the fluidic behavior on lateral confinement by placing side-walls on the planar plug nozzle through experiments. The study involves two cases of nozz…