A natural laminar-turbulent transition model compatible with Computation Fluid Dynamics is presented. This model accounts for longitudinal transition mechanisms (i.e. Tollmien-Schlichting induced transition) thanks to systematic stability computation on similar boundary profiles from Mach zero to four both on adiabatic and isothermal wall. The model embeds as well the so-called “C1-criterion” for transverse transition mechanisms (i.e. cross-flow waves induced transition). The transition model is written under transport equations formalism and has been implemented in the solver elsA (ONERA-Airbus-Safran property). Validations are performed on three dimensional configurations and comparisons are shown against a database method for natural tra...
A computationally-efficient method based on Kalman filtering is introduced to capture “on the fly” t...
An experimental investigation on the flow topology and performance of a rotor operating at low Reyn...
This work is motivated by the need for low-order aerodynamic models to predict accurately the effect...
A laminar–turbulent transition model is presented. The model accounts for longitudinal transition me...
The present investigation targets the generation of airfoil trailing-edge broadband noise that arise...
This article presents the large-eddy simulation (LES) of a low-pressure turbine (LPT) nozzle guide v...
Classical RANS turbulence models have known deficiencies when applied to jets in crossflow. Identify...
Turbulent-flow interactions with the outlet guide vanes are known to mainly contribute to broadband-...
The in-house linear stability solver of ONERA has been extended to rotating frames. The theoretical ...
In gas turbine, multi-stage row blading and technological effects can exhibit significant difference...
International audienceThis work is part of the study of the turbulent mixture produced by the Richtm...
The streamwise breathing motion of the separation bubble, triggered by the shock wave/boundary layer...
The heat equation with boundary control and observation can be described by means of three different...
In the framework of an optimization study of a Zero-Net-Mass-Flux fluidic, synthetic jet actuator, b...
A common idea in the PinT community is that Parareal, one of the most popular time-parallel algorith...
A computationally-efficient method based on Kalman filtering is introduced to capture “on the fly” t...
An experimental investigation on the flow topology and performance of a rotor operating at low Reyn...
This work is motivated by the need for low-order aerodynamic models to predict accurately the effect...
A laminar–turbulent transition model is presented. The model accounts for longitudinal transition me...
The present investigation targets the generation of airfoil trailing-edge broadband noise that arise...
This article presents the large-eddy simulation (LES) of a low-pressure turbine (LPT) nozzle guide v...
Classical RANS turbulence models have known deficiencies when applied to jets in crossflow. Identify...
Turbulent-flow interactions with the outlet guide vanes are known to mainly contribute to broadband-...
The in-house linear stability solver of ONERA has been extended to rotating frames. The theoretical ...
In gas turbine, multi-stage row blading and technological effects can exhibit significant difference...
International audienceThis work is part of the study of the turbulent mixture produced by the Richtm...
The streamwise breathing motion of the separation bubble, triggered by the shock wave/boundary layer...
The heat equation with boundary control and observation can be described by means of three different...
In the framework of an optimization study of a Zero-Net-Mass-Flux fluidic, synthetic jet actuator, b...
A common idea in the PinT community is that Parareal, one of the most popular time-parallel algorith...
A computationally-efficient method based on Kalman filtering is introduced to capture “on the fly” t...
An experimental investigation on the flow topology and performance of a rotor operating at low Reyn...
This work is motivated by the need for low-order aerodynamic models to predict accurately the effect...