Articles written in Sadhana
Volume 40 Issue 3 May 2015 pp 627-652 Section I – Fluid Mechanics and Fluid Power (FMFP)
Functions and conservation as well as subsidiary equations in
Volume 40 Issue 3 May 2015 pp 819-833 Section I – Fluid Mechanics and Fluid Power (FMFP)
The present work on downward injection of
Volume 40 Issue 8 December 2015 pp 2367-2379
In this work, we present detailed particle image velocimetry (PIV) based investigation of wake structure of a pitching airfoil. PIV measurements have been carried out for NACA0015 airfoil at Re = 2900 with reduced frequency range of 1.82–10.92 and pitching angle of 5°. Two different wake structures (reverse Kármán shedding and deflected vortex shedding) are observed over this parameter range. The vorticity decreases substantially over a distance of two chord-lengths. The velocity profile indicates a jet-like flow downstream of the airfoil. It is shown that the jet-like flow downstream of the airfoil is however not a sufficient condition for the generation of thrust. The vortex strength is found to be invariant of the pitching frequency. Certain differences from the reported results are noted, which may be because of difference in the airfoil shape. These results can help improve understanding of the flow behavior as the low Reynolds number range is not well studied.
Volume 42 Issue 4 April 2017 pp 585-595
Fish-like undulating body was proposed as an efficient propulsion system, and various mechanisms of thrust generation in this type of propulsion are found in the literature—separately for undulating and pitching fishes/foil. The present work proposes a unified study for undulating and pitching foil, by varying wavelength l (from 0.8 to 8.0) of a wave traveling backwards over the NACA0012 hydrofoil in a free-stream flow; the larger wavelength is shown to lead to the transition from the undulating motion to pitching motion. The effect ofwavelength of undulation is studied numerically at a Reynolds number Re=4000, maximum amplitude of undulation Amax 0:1 and non-dimensional frequency of undulation St=0:4, using level-set immersedboundary-method based in-house 2D code. The Navier–Stokes equation governing the fluid flow is solved using a fully implicit finite-volume method, while level-set equation governing the movement of the hydrofoil is solved using an explicit finite-difference method. It is presented here that the thrust generation mechanism for the low wavelength case undulating (l=0.8) foil is different from the mechanism for the high wavelength pitching foil. With increasing wavelength, mean thrust coefficient of the undulating foil increases and asymptotes to value for the pure pitching foil. Furthermore, the ratio of maximum thrust coefficient to maximum lateral force coefficient is found to be larger for the smaller wavelength undulating foil as compared with the larger wavelength pitching foil.
Volume 46 All articles Published: 18 August 2021 Article ID 0170
The present work proposes a cut-cell-based Direct Simulation Monte Carlo (DSMC) solver, for computing rarefied flows around complex geometries on Cartesian grids, wherein analytical expression for the surface of the immersed boundary (IB) is considered to evaluate cut-cell volume as well as to implement the particle–boundary interactions. Consequently the proposed DSMC solver models an accurate collision rate in the cut cells and ensures an analytically expressed IB-based implementation of the boundary conditions at thesurface of the immersed geometry, as in the IB methods for the continuum flows. Performance of the present Cartesian cut-cell-based DSMC solver is tested on a variety of rarefied gas flows around three complex geometries (cylinder, NACA 0012 airfoil and double-wedge airfoil) for various flow speeds (ranging from
Volume 48 All articles Published: 7 February 2023 Article ID 0022
Adaptive interface-Mesh un-Refinement (AiMuR) based Sharp-Interface
Level-Set-Method (SILSM) is proposed for both uniform and non-uniform Cartesian-Grid.
The AiMuR involves interface location based dynamic un-refinement (with
merging of the four control volumes) of the Cartesian grid away from theinterface.
The un-refinement is proposed for the interface solver only. A detailed numerical methodology is presented
for the AiMuR and ghost-fluid method based SI-LSM. Advantage of the novel as compared
to the traditional SI-LSM is demonstrated with a detailed qualitative as well as quantitative
performance study, involving the SI-LSMs on both coarse grid and fine grid, for three sufficiently
different two-phase flow problems:dam break, breakup of a liquid jet and drop coalescence.
A superior performance of AiMuR based SI-LSM is demonstrated - the AiMuR on a coarser non-uniform