Add to ORKGA detailed computational aeroacoustic analysis of a high-lift flow field is performed. Time-accurate Reynolds Averaged Navier-Stokes (RANS) computations simulate the free shear layer that originates from the slat cusp. Both unforced and forced cases are studied. Preliminary results show that the shear layer is a good amplifier of disturbances in the low to mid-frequency range. The Ffowcs-Williams and Hawkings equation is solved to determine the acoustic field using the unsteady flow data from the RANS calculations. The noise radiated from the excited shear layer has a spectral shape qualitatively similar to that obtained from measurements in a corresponding experimental study of the high-lift system
A companion paper by Khorrami et al demonstrates the feasibility of simulating the (nominally) self-...
In numerical computation of aerodynamic noises, the solution accuracy of flow fields has an obvious ...
Three dimensional time-accurate simulations on a leading-edge slat and wing combination were carried...
Unsteady computational simulations of a multi-element, high-lift configuration are performed. Emphas...
An acoustic analysis based on the Ffowcs Williams and Hawkings equation was performed for a high-lif...
High-lift devices on modern airliners are a major contributor to overall airframe noise. In this pap...
This paper extends our previous computations of unsteady flow within the slat cove region of a multi...
High-lift devices on modern airliners are a major contributor to overall airframe noise. In this pap...
In previous work a RANS based simulation technique for the simulation of broadband slat noise was es...
The flow field and the acoustic field of a high-lift configuration consisting of a slat and a main w...
Global hybrid RANS/LES simulations were used for computing the turbulent flow around a three-element...
Slat Noise simulations are carried out for a high-lift airfoil. A low-cost Computational Aeroacou...
A hybrid RANS/LES modeling approach is used for simulating the turbulent flow around a three-element...
The slat noise from the 30P30N high-lift system has been computed using a computational fluid dynami...
In this paper the aeroacoustics of leading-edge slat devices in a high-lift configuration are invest...
A companion paper by Khorrami et al demonstrates the feasibility of simulating the (nominally) self-...
In numerical computation of aerodynamic noises, the solution accuracy of flow fields has an obvious ...
Three dimensional time-accurate simulations on a leading-edge slat and wing combination were carried...
Unsteady computational simulations of a multi-element, high-lift configuration are performed. Emphas...
An acoustic analysis based on the Ffowcs Williams and Hawkings equation was performed for a high-lif...
High-lift devices on modern airliners are a major contributor to overall airframe noise. In this pap...
This paper extends our previous computations of unsteady flow within the slat cove region of a multi...
High-lift devices on modern airliners are a major contributor to overall airframe noise. In this pap...
In previous work a RANS based simulation technique for the simulation of broadband slat noise was es...
The flow field and the acoustic field of a high-lift configuration consisting of a slat and a main w...
Global hybrid RANS/LES simulations were used for computing the turbulent flow around a three-element...
Slat Noise simulations are carried out for a high-lift airfoil. A low-cost Computational Aeroacou...
A hybrid RANS/LES modeling approach is used for simulating the turbulent flow around a three-element...
The slat noise from the 30P30N high-lift system has been computed using a computational fluid dynami...
In this paper the aeroacoustics of leading-edge slat devices in a high-lift configuration are invest...
A companion paper by Khorrami et al demonstrates the feasibility of simulating the (nominally) self-...
In numerical computation of aerodynamic noises, the solution accuracy of flow fields has an obvious ...
Three dimensional time-accurate simulations on a leading-edge slat and wing combination were carried...