Our previous studies have indicated that 2D, time accurate computations based on a pseudo-laminar zonal model of the slat cove region (within the framework of the Reynolds-Averaged Navier-Stokes equations) are inadequate for predicting the full unsteady dynamics of the slat cove flow field. Even though such computations could capture the large-scale, unsteady vorticity structures in the slat cove region without requiring any external forcing, the simulated vortices were excessively strong and the recirculation zone was unduly energetic in comparison with the PIV measurements for a generic high-lift configuration. To resolve this discrepancy and to help enable physics based predictions of slat aeroacoustics, the present paper is focused on 3...
The unsteady flow around the leading edge slat of a three-element high lift aerofoil configuration h...
Slat Noise simulations are carried out for a high-lift airfoil. A low-cost Computational Aeroacou...
this paper will conform to the schematic of the experimental setup shown in Fig. 1. The view in Fig....
This paper extends our previous computations of unsteady flow within the slat cove region of a multi...
A companion paper by Khorrami et al demonstrates the feasibility of simulating the (nominally) self-...
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...
High-lift devices on modern airliners are a major contributor to overall airframe noise. In this pap...
High-lift devices on modern airliners are a major contributor to overall airframe noise. In this pap...
An experimental investigation of the unsteady flow field inside a slat cove was performed to identif...
A comprehensive computational and experimental study has been performed at the NASA Langley Research...
Experimental measurements were carried out to assess the aeroacoustic characteristics of 30P30N airf...
The slat noise from the 30P30N high-lift system has been computed using a computational fluid dynami...
We investigate the slat narrowband peak noise generating mechanism. Unsteady flow data were generate...
The flow field and the acoustic field of a high-lift configuration consisting of a slat and a main w...
The unsteady flow around the leading edge slat of a three-element high lift aerofoil configuration h...
Slat Noise simulations are carried out for a high-lift airfoil. A low-cost Computational Aeroacou...
this paper will conform to the schematic of the experimental setup shown in Fig. 1. The view in Fig....
This paper extends our previous computations of unsteady flow within the slat cove region of a multi...
A companion paper by Khorrami et al demonstrates the feasibility of simulating the (nominally) self-...
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...
High-lift devices on modern airliners are a major contributor to overall airframe noise. In this pap...
High-lift devices on modern airliners are a major contributor to overall airframe noise. In this pap...
An experimental investigation of the unsteady flow field inside a slat cove was performed to identif...
A comprehensive computational and experimental study has been performed at the NASA Langley Research...
Experimental measurements were carried out to assess the aeroacoustic characteristics of 30P30N airf...
The slat noise from the 30P30N high-lift system has been computed using a computational fluid dynami...
We investigate the slat narrowband peak noise generating mechanism. Unsteady flow data were generate...
The flow field and the acoustic field of a high-lift configuration consisting of a slat and a main w...
The unsteady flow around the leading edge slat of a three-element high lift aerofoil configuration h...
Slat Noise simulations are carried out for a high-lift airfoil. A low-cost Computational Aeroacou...
this paper will conform to the schematic of the experimental setup shown in Fig. 1. The view in Fig....