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Sparsh Sharma

Publications and source records attributed to Sparsh Sharma.

4 recordsLinked to original sources

A transport geometry of acoustic analogies:exact holonomy of source re-attribution and its observable consequences

The source term of an acoustic analogy is not unique: different rearrangements of the Navier-Stokes equations attribute the same radiated sound to different apparent sources. Although this non-uniqueness has long been recognised, it has never been given a quantitative structure. We provide one by organising acoustic analogies into a fibre-like family over the space of effective media and defining transport between analogies through unique frequency-preserving, rotation-free linear space-time maps. Three exact results follow. First, the classical family of convected analogies is not closed under transport: successive uniform-flow regaugings generate effective media with anisotropic sound-speed tensors, recovering the generalised media introduced by Goldstein. Second, the discrete holonomy of analogy transport is obtained in closed form. It consists of an exact spectral dilation and a rotation that vanishes to fourth order in Mach number; transport becomes singular on a sonic horizon in analogy space. Third, in the continuum limit the boost sector is flat, while curvature is confined to anisotropy directions and is given by the commutator of sound-speed-tensor increments. The geometry does not imply any change in the physical sound field: all exact analogies yield the same far field. Its significance is operational. When an approximate source model is transported between analogies, as commonly occurs in hybrid prediction methods, the resulting far-field predictions acquire an exact, parameter-free bias consisting of a rigid spectral dilation and directivity rotation. An exact far-field law for anisotropic media extends these results to open transport paths. All identities are verified symbolically and numerically.

physics.flu-dyn

Strain-coupled one-dimensional turbulence for rapid distortion

The distortion of turbulence by mean strain - through component amplification, pressure-mediated redistribution and spectral rescaling - is central to flows ranging from wind-tunnel contractions to stagnation regions near lifting surfaces. Capturing this process economically remains difficult: scale-resolving simulation is expensive, linear rapid-distortion theory omits nonlinear relaxation over finite strain, and second-moment closures discard spectral information. We present a strain-coupled formulation of one-dimensional turbulence (ODT) that evolves strained turbulence with one-dimensional scale resolution at low computational cost. Mean-strain production is imposed as a continuous forcing of the line velocity, the rapid pressure-strain contribution is introduced as an energy-conserving redistribution operator consistent with homogeneous rapid-distortion theory, and scale compression is represented by dilatation of the ODT domain. The model predicts a broadband distorted spectrum that departs from the rigid spectral translation of linear theory at a strain-to-turbulence ratio of approximately 0.8, where rapid distortion and nonlinear eddy dynamics are both active. Under axisymmetry of the undistorted turbulence about the ODT line, the nonlocal three-dimensional rapid pressure-strain integral reduces to a closed single-line functional. The formulation reproduces rapid-distortion theory at onset and quantitatively captures the Reynolds-stress anisotropy trends of Lee and Reynolds (1985).

physics.flu-dyn

Effect of geometric parameters on the noise generated by rod-airfoil configuration

This paper investigates the effect of the geometric parameters -- rod diameter and the distance between the rod and the airfoil -- on the noise generated by rod-airfoil configuration using experimental and numerical techniques. The numerical simulations are carried out using the low-dissipation up-wind scheme and the Delayed-Detached-Eddy Simulation (DDES) approach with Shear-Layer Adapted (SLA) sub-grid length scale (SGS) for a faster transition between RANS and LES. A dual-time stepping strategy, leading to second-order accuracy in space and time, is followed. The Ffowcs-Williams and Hawkings (FWH) technique is used to post-process the pressure fluctuations to predict the far~field acoustics. A corresponding detailed experimental analysis, carried out using phased microphone array techniques in the aeroacoustic wind tunnel at the Brandenburg Technical University at Cottbus, is used for the validation of the numerical method. The key objective of the analysis is to examine the influence of the parameters of the configuration on the noise generation. The results show reasonable agreement with the experimental data in terms of far-field acoustics.

physics.flu-dyn

On a lower-order framework for jet noise prediction based on one-dimensional turbulence

Noise prediction requires the resolution of relevant acoustic sources on all scales of a turbulent flow. High-resolution direct numerical and large-eddy simulation would be ideal but both are usually too costly despite developments in high performance computing. Lower-order modeling approaches are therefore of general interest. A crucial but standing problem for accurate predictive modeling is the estimation of missing noise from the modeled scales. In this paper we address this problem by presenting a novel lower-order framework that couples the one-dimensional turbulence model to the Ffowcs-Williams and Hawkings approach for prediction of the far-field noise of a subsonic turbulent round jet.

physics.flu-dyn