John Sheridan

ORCID: 0000-0001-9164-2436
Publications
Citations
Views
---
Saved
---
About
Contact & Profiles
Research Areas
  • Fluid Dynamics and Vibration Analysis
  • Wind and Air Flow Studies
  • Aerodynamics and Fluid Dynamics Research
  • Fluid Dynamics and Turbulent Flows
  • Molecular Spectroscopy and Structure
  • Vibration and Dynamic Analysis
  • Advanced Chemical Physics Studies
  • Inorganic Fluorides and Related Compounds
  • Biomimetic flight and propulsion mechanisms
  • Atmospheric Ozone and Climate
  • Wind Energy Research and Development
  • Spectroscopy and Laser Applications
  • Fluorine in Organic Chemistry
  • Aerodynamics and Acoustics in Jet Flows
  • Lattice Boltzmann Simulation Studies
  • Aerospace Engineering and Energy Systems
  • Fluid Dynamics Simulations and Interactions
  • Microwave-Assisted Synthesis and Applications
  • Heat and Mass Transfer in Porous Media
  • Fluid dynamics and aerodynamics studies
  • Inorganic and Organometallic Chemistry
  • Aeolian processes and effects
  • Various Chemistry Research Topics
  • Tropical and Extratropical Cyclones Research
  • Molecular spectroscopy and chirality

Monash University
2013-2022

New York University Press
2018

Cambridge University Press
2018

Harvard University Press
2018

Chitose Institute of Science and Technology
2018

Bridge University
2018

University of Cambridge
2018

Google (United States)
2018

Indian Institute of Technology Bombay
2016

IITB-Monash Research Academy
2016

Abstract This study investigates the free transverse flow-induced vibration (FIV) of an elastically mounted low-mass-ratio square cylinder in a stream, at three different incidence angles: ${{\alpha }}=0^\circ $ , $20^\circ and $45^\circ . geometric setup presents body with angle attack, sharp corners some afterbody, therefore is generic that can be used to investigate wide range FIV phenomena. A recent by Nemes et al. ( J. Fluid Mech. vol. 710, 2012, pp. 102–130) provided broad overview...

10.1017/jfm.2014.167 article EN Journal of Fluid Mechanics 2014-04-23

10.1016/0894-1777(95)00098-4 article EN Experimental Thermal and Fluid Science 1996-02-01

The first page of this article is displayed as the abstract.

10.1039/tf9635902661 article EN Transactions of the Faraday Society 1963-01-01

Abstract This study examines the influence of angle attack a square section cylinder on cylinder’s flow-induced vibration, where direction vibration is transverse to oncoming flow. Our experiments, which traversed velocity–angle parameter space in considerable breadth and depth, show that low-mass ratio body can undergo combinations both vortex-induced galloping. When has an makes it symmetric flow, such as when assumes or diamond orientation, two mechanisms remain independent. However,...

10.1017/jfm.2012.353 article EN Journal of Fluid Mechanics 2012-08-31

Abstract Previous studies investigating the effect of aspect ratio ( $\mathit{AR}$ ) for insect-like regimes have reported seemingly different trends in aerodynamic forces, however no detailed flow observations been made. In this study, and Reynolds number on structures over wings is explored using a numerical model an altered fruit fly wing revolving at constant angular velocity. Increasing 2.91 resulted development dual leading-edge vortex (LEV) structure, increasing fixed generated same...

10.1017/jfm.2012.565 article EN Journal of Fluid Mechanics 2013-02-01

10.1016/j.jweia.2014.09.004 article EN Journal of Wind Engineering and Industrial Aerodynamics 2014-09-29

Abstract While the wake of a circular cylinder and, to lesser extent, normal flat plate have been studied in considerable detail, wakes elliptic cylinders not received similar attention. However, from first two bodies considerably different characteristics, terms three-dimensional transition modes, and near- far-wake structure. This paper focuses on cylinders, which span these disparate cases. The Strouhal number drag coefficient variations with Reynolds are documented for two-dimensional...

10.1017/jfm.2014.314 article EN Journal of Fluid Mechanics 2014-06-24

10.1016/j.jweia.2014.09.007 article EN Journal of Wind Engineering and Industrial Aerodynamics 2014-11-29

Using equilibrium and nonequilibrium molecular dynamic simulations, we found that engineering the strain on graphene planes forming a channel can drastically change interfacial friction of water transport through it. There is sixfold stress when changes from -10% to 10%. Stretching walls increases shear stress, while compressing reduces Detailed analysis structure reveals essential roles potential energy barrier structural commensurateness between solid first layer. Our results suggest an...

10.1103/physreve.84.056329 article EN Physical Review E 2011-11-28

L. F. Thomas, E. I. Sherrard and J. Sheridan, Trans. Faraday Soc., 1955, 51, 619 DOI: 10.1039/TF9555100619

10.1039/tf9555100619 article EN Transactions of the Faraday Society 1955-01-01

A numerical study of the flow-induced vibration two elastically mounted cylinders in tandem and staggered arrangements at Reynolds number $Re=200$ is presented. The cylinder centres are set a streamwise distance 1.5 diameters, placing rear near-wake region front for arrangement. cross-stream or lateral offset varied between 0 5 diameters. identical, with same elastic mounting, constrained to oscillate only cross-flow direction. variation flow behaviours examined static mountings range spring...

10.1017/jfm.2017.673 article EN Journal of Fluid Mechanics 2017-11-02

Measurements of the $J=1\ensuremath{\rightarrow}2$ rotational transitions ${\mathrm{N}}^{14}$${\mathrm{F}}_{3}$ and ${\mathrm{N}}^{15}$${\mathrm{F}}_{3}$ yield following molecular nuclear properties. For ${\mathrm{N}}^{14}$${\mathrm{F}}_{3}$, ${\mathrm{B}}_{0}$=10,680.96 Mc/sec., ${I}_{\mathrm{B}}=78.5475\ifmmode\times\else\texttimes\fi{}{10}^{\ensuremath{-}40}$ g ${\mathrm{cm}}^{2}$; for ${\mathrm{N}}^{15}$${\mathrm{F}}_{3}$, ${\mathrm{B}}_{0}$=10,629.35...

10.1103/physrev.79.513 article EN Physical Review 1950-08-01

The pure rotational spectra of trifluoromethyl bromide, iodide, and cyanide have been studied in the microwave region. B0 values Mc/sec were determined as follows: 2098.06 for CF3Br79; 2078.50 CF3Br81; 1523.23 CF3I; 2945.535 CF3CN14; 2855.859 CF3CN15. nuclear quadrupole couplings, eQq, are Mc/sec: 619 Br79; 517 Br81; −2150 I127; −4.70 N14. With any reasonable assumption bond angles, dCF is found to be 1.33±0.015A each molecule. other distances depend more strongly on angles. ∠FCF assumed...

10.1063/1.1700499 article EN The Journal of Chemical Physics 1952-04-01

From measurements of pure rotational transitions in the microwave region following B0 values Mc/sec were determined: 4594.25±0.04 for PO16F3, 4395.27±0.20 PO18F3, 2657.63±0.04 PS32F3, 2614.73±0.04 PS33F3, 2579.77±0.04 PS34F3, 2015.20±0.05 PO16Cl335, 1932.38±0.08 PO16Cl337, 1402.64±0.05 PS32Cl235, 1355.72±0.05 PS32Cl337, 1370.13±0.05 PS34Cl335. With aid electron diffraction results molecular structures have been determined as follows: POF3, dPO=1.45±0.03A, dPF=1.52±0.02A and ∠FPF=102.5°±2°;...

10.1063/1.1700162 article EN The Journal of Chemical Physics 1952-01-01

The wake states from a circular cylinder undergoing controlled sinusoidal oscillation transverse to the free stream are examined. As frequency of passes through natural Kármán there is transition between two distinctly different states: low- and high-frequency states. corresponds change in structure near also characterized by jump phase amplitude both total vortex lift. Over range flow parameters studied exhibit number universal features. phases lift drag forces have characteristic values...

10.1017/s0022112005005197 article EN Journal of Fluid Mechanics 2005-08-17

10.1006/jfls.2000.0363 article EN Journal of Fluids and Structures 2001-04-01

Flow past a cylinder beneath free surface gives rise to fundamental classes of nearwake structure that are distinctly different from the wake completely submerged cylinder. A central feature is generation vorticity layer due to: localized separation, in form small-scale breaking free-surface wave; or complete separation surface. This appears adjacent cylinder, thereby forming jet-like flow. It shown instantaneous flux on either side this jet rapidly balanced immediately after onset

10.1017/s002211209600328x article EN Journal of Fluid Mechanics 1997-01-10

The stable molecular conformations of methyl-fluoroformate, -propiolate, -cyanoformate, -acrylate (cis) and -acetate have been shown to be planar, for the latter four compounds cis ester skeleton has established. Barriers internal rotation methyl group were measured from splittings microwave lines each compound. [XCOOCH3; X = F, V3= 1077; HCC, 1266; CN, 1172; CH3, 1215; CH2CH, 1220 (values V3 in cal/mol).] For acetate a value 307 ± 50 cal/mol acetyl was calculated spectrum CD3COOCD3. dipole...

10.1039/tf9716700922 article EN Transactions of the Faraday Society 1971-01-01
Coming Soon ...