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Jagadeesh G

Publications and source records attributed to Jagadeesh G.

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

Insights into the shockwave attenuation in miniature shock tubes

Miniature shock tubes are finding growing importance in a variety of interdisciplinary applications. There is a lack of experimental data to validate the existing shock tube flow models that explain the shockwave attenuation in pressure-driven miniature shock tubes. This paper gives insights into the shock formation and shock propagation phenomena in miniature shock tubes of 2mm, 6mm, and 10mm square cross-sections operated at diaphragm rupture pressure ratios in the range 5-25 and driven section initially at ambient conditions. Pressure measurements and visualization studies are carried out in a new miniature table-top shock tube system using nitrogen and helium as driver gases. The experimental findings are validated using a shock tube model explained in terms of two regions; (1) The shock formation region, dominated by wave interactions due to the diaphragm's finite rupture time. (2) The shock propagation region, where the shockwave attenuation occurs mainly due to wall effects and boundary layer growth. Correlations to predict the variation of shock Mach number in the shock formation region and shock propagation region work well for the present findings and experimental data reported in the literature. Similar flow features are observed in the shock tubes at the same dimensionless time stamps. The formation of the planar shock front scales proportionally with the diameter of the shock tube. The peak Mach number attained by the shockwave is higher as the shock tube diameter increases.

physics.flu-dyn