activity
20242026
collaborators

6 papers

physics.flu-dyn2026

Supervised machine learning of compressible flow past a rotating cylinder

Sanjeev Kumar, Santosh Kumar, Aditi Sengupta

High-fidelity numerical simulations of compressible flow past a rapidly rotating cylinder are used to investigate the evolution of aerodynamic loads and flow instability over a wid…

physics.flu-dyn2026

Separation induced transition in a low pressure turbine under varying compressibility

Priya Pal, Abhijeet Guha, Aditi Sengupta

The present study investigates influence of compressibility on separation induced transition in a low pressure turbine cascade using high fidelity direct numerical simulations of t…

physics.flu-dyn2025

Role of varying Reynolds number for flow past a rotating cylinder at high rotation rate

Aditi Sengupta, Santosh Kumar, Sanjeev Kumar

The present study reports comprehensive bifurcation analysis of flow past a rotating cylinder at a fixed rotation rate by varying free-stream Reynolds number () from 1…

physics.flu-dyn2025

Spatio-temporal pulse propagation during highly-resolved onset of Rayleigh-Taylor and Kelvin-Helmholtz Rayleigh-Taylor instabilities

Bhavna Joshi, Aditi Sengupta, Yassin Ajanif +1

The present study explores the onset of the Rayleigh-Taylor instability (RTI) and Kelvin-Helmholtz Rayleigh-Taylor instability (KHRTI) with highly-resolved direct numerical simulat…

physics.flu-dyn2024

Comparing design and off-design aerodynamic performance of a natural laminar airfoil

Aditi Sengupta, Abhijeet Guha

Natural laminar flow airfoils are essential technologies designed to reduce drag and significantly enhance aerodynamic performance. A notable example is the SHM1 airfoil, created t…

physics.flu-dyn2024

Effect of Gaussian wake amplitude on wake-induced transition for a T106A low pressure turbine cascade

Aditi Sengupta

The wake-induced transition on the suction surface of a T106A low-pressure turbine (LPT) blade is investigated through a series of implicit large eddy simulations, solving the two-…