CleanEra: A Collection of Research Projects for Sustainable Aviation

Laminar-Turbulent Transition in Swept-Wing Flows with a Supercritical Forward-Facing Step

Numerical Study on Control of Tollmien-Schlichting Waves Using Plasma Actuators

Plasmas for Transition Delay

Flow visualization of swept wing boundary layer transition

A two-parameter method for eN transition prediction

Experimental Study on the Body Force Field of Dielectric Barrier Discharge Actuators

Secondary instabilities in swept-wing boundary layers: Direct Numerical Simulations and BiGlobal stability analysis

Experimental Investigation of Isolated Roughness Induced Transition in a Swept Wing Boundary Layer

Sensitivity of crossflow surfacetransitionroughnessto free-stream conditions and

PIV analysis of skin friction and coherent structures in turbulent drag reduction regimes

Linear and Nonlinear Stability Analysis of a Three-Dimensional Boundary Layer over a Hump

The Near-Wake of Super-Critical Discrete Roughness Elements on Swept Wings

Control of fluid flows using multivariate spline reduced order models

Two-phase wake-mixing layer flow past a splitter plate: an experimental investigation

Stability of Swept Wing Boundary Layers under Non-Adiabatic Wall Conditions

Swept Transition Experimental Platform (STEP)

Optimization of Tollmien-Schlichting waves control: comparison between a deep reinforcement learning and particle swarm optimization approach

Experimental Investigation on Receptivity of Crossflow Instability to Discrete Roughness Amplitude and Location

Mechanisms of interaction between stationary crossflow instabilities and forward-facing steps