Shock waves

Direct numerical simulations of hypersonic shock-turbulence interactions

Oral presentation in the 76th Annual Meeting of the American Physical Society’s Division of Fluid Dynamics

Direct Numerical Simulations and Linear Analysis for Hypersonic Shock-Turbulence Interaction in Air

Flash talk in the 4th Spanish HPC Combustion Workshop

Development of a wide-spectrum thermochemical code with application to planar reacting and non-reacting shocks

The recent scientific and technological advancements have underscored the critical necessity for reliable, robust, and efficient numerical codes capable of predicting the chemical composition and properties of complex mixtures at chemical …

Combustion Toolbox: An open-source thermochemical code for gas- and condensed-phase problems involving chemical equilibrium

We present a new thermochemical code---hereafter referred to as Combustion Toolbox (CT)---for the solution of problems that involve chemical equilibrium of gas- and condensed-phase species. The kernel of the code is based in the theoretical framework …

Linear analysis on shock-turbulence interaction implemented with the Combustion Toolbox

In this seminar, we present the development of an in-house thermochemical code ---hereafter referred to as Combustion Toolbox (CT)--- for the solution of problems that involve chemical equilibrium of gas- and condensed-phase species. The …

Linear Theory of Hypersonic Shocks Interacting with Turbulence in Air

Oral presentation in the 2023 AIAA SciTech Forum

Direct Numerical Simulations and Linear Analysis for Hypersonic Shock-Turbulence Interaction in Air

Amplificación de la turbulencia a través de una onda de choque en régimen hipersónico

Short talk (b) presented in the 9th ''Congreso Nacional de I+D en Defensa y Seguridad''.

Theory of turbulence augmentation across hypersonic shock waves in air

The interaction between a weakly turbulent free stream of air and a hypersonic shock wave is investigated theoretically by using linear interaction analysis (LIA). The perturbation-free jump conditions across the shock are computed using Combustion …

Theory of turbulence augmentation across hypersonic shock waves

The interaction between a weakly turbulent free stream and a hypersonic shock wave is investigated theoretically by using linear interaction analysis (LIA). Modified Rankine-Hugoniot jump conditions that account for dissociation and vibrational …