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Research article

First published 2024-9

Intermittency transition to azimuthal instability in a turbulent annular combustor

Samarjeet Singh, Ramesh S. Bhavi, Midhun P. Raghunath [...]

International Journal of Spray and Combustion Dynamics

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Research article

First published 2021-3

H ∞ loop-shaping control of azimuthal combustion instabilities in annular combustors

Sheng Feng, Jingxuan Li

Journal of Low Frequency Noise,Vibration and Active Control

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Research article

First published 2024-6

Longitudinal and azimuthal thermo-acoustic instabilities in an industrial gas turbine combustor operating at elevated pressure

Daniel Fredrich, William P Jones, Andrew J Marquis [...]

International Journal of Spray and Combustion Dynamics

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Research article

First published 2024-5

Investigation of inlet flow influenced on the first rotor flow instability at blade non-synchronous vibration state

Hongwei Ma, Zengzeng Wang, Xiang He [...]

Proceedings of the Institution of Mechanical Engineers,Part G: Journal of Aerospace Engineering

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Research article

First published 2009-1

A Tool to Study Azimuthal Standing and Spinning Modes in Annular Combustors

C. Sensiau, F. Nicoud, T. Poinsot

International Journal of Aeroacoustics

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Research article

First published 2011-1

Instabilities of Highly Anisotropic Spinning Disks

Ciprian D. Coman

Mathematics and Mechanics of Solids

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Research article

First published 2025-9

Study of the control mechanism on combustion instabilities using perforated injector mounting surface

Lei Qin, Guangyu Zhang, Xiaoyu Wang [...]

International Journal of Spray and Combustion Dynamics

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Research article

First published 1977-4

‘Wavy’ Modes of Instability in the Flow between Eccentric Rotating Cylinders

P. H. Markho, C. D. Jones, F. R. Mobbs

Journal of Mechanical Engineering Science

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Research article

First published 2009-5

A Study of the Correlation of Large-Scale Structure Dynamics and Far-Field Radiated Noise in an Excited Mach 0.9 Jet

Jeff Kastner, Jin-Hwa Kim, Mo Samimy

International Journal of Aeroacoustics

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Research article

First published 2016-4

The effect of low lobe count chevron nozzles on supersonic jet screech

Nathan J Humphrey, Daniel Edgington-Mitchell

International Journal of Aeroacoustics

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