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Srisha M. V. Rao

Publications and source records attributed to Srisha M. V. Rao.

2 recordsLinked to original sources

Kinematics of Single-Winged Spinning Seeds: A Study on Mahogany and Buddha Coconut Samaras

This study investigates the steady-state kinematics of single-winged spinning samaras and re-evaluates the simplifying assumptions commonly used in existing theoretical models. High-speed imaging was employed to quantify key parameters, including descent velocity, rotational speed, coning angle, pitching motion, and the precessional trajectory of the center of mass. The results show that all measured parameters exhibit significant temporal variation, contradicting the long-standing assumption that these quantities remain constant in steady-state flight. This variability reveals that commonly used steady-state simplifications in previous studies may overlook essential aerodynamic mechanisms governing natural samara descent. Despite this complexity, the observed sinusoidal variations in pitch, cone angle, and translational velocity, together with the nearly linear rotation rate, provide a physically grounded basis for reformulating the governing nonlinear differential equations into a simplified algebraic form. Such experimentally validated harmonic representations offer a more realistic alternative to traditional steady-state assumptions. The visualized trajectories of the center of mass, root tip, wingtip quarter-chord point, and wingtip trailing edge reveal the inherently coupled nature of samara motion and highlight the need for future experiments that capture full three-dimensional kinematics. Overall, this work advances the understanding of samara aerodynamics by emphasizing the importance of natural variability while identifying a tractable path toward more accurate modelling frameworks.

physics.flu-dyn↗

Elliptic supersonic jet morphology manipulation using sharp-tipped lobes

Elliptic nozzle geometry is attractive for mixing enhancement of supersonic jets. However, jet dynamics, such as flapping, gives rise to high-intensity tonal sound. We experimentally manipulate the supersonic elliptic jet morphology by using two sharp-tipped lobes. The lobes are placed on either end of the minor axis in an elliptic nozzle. The design Mach number and the aspect ratio of the elliptic nozzle and the lobed nozzle are 2.0 and 1.65. The supersonic jet is exhausted into ambient at almost perfectly expanded conditions. Time-resolved schlieren imaging, longitudinal and cross-sectional planar laser Mie-scattering imaging, planar Particle Image Velocimetry, and near-field microphone measurements are performed to assess the fluidic behavior of the two nozzles. Dynamic Mode and Proper Orthogonal Decomposition (DMD and POD) analysis are carried out on the schlieren and the Mie-scattering images. Mixing characteristics are extracted from the Mie-scattering images through the image processing routines. The flapping elliptic jet consists of two dominant DMD modes, while the lobed nozzle has only one dominant mode, and the flapping is suppressed. Microphone measurements show the associated noise reduction. The jet column bifurcates in the lobed nozzle enabling a larger surface contact area with the ambient fluid and higher mixing rates in the near-field of the nozzle exit. The jet width growth rate of the two-lobed nozzle is about twice as that of the elliptic jet in the near-field, and there is a 40\% reduction in the potential core length. Particle Image Velocimetry (PIV) contours substantiate the results.

physics.flu-dyn↗