Dynamical systems approach to study thermoacoustic transitions in a liquid rocket combustor-Reference-Cited by-同舟云学术

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Dynamical systems approach to study thermoacoustic transitions in a liquid rocket combustor

Published:2019-10 Issue:10 Volume:29 Page:103115
ISSN:1054-1500
Container-title:Chaos: An Interdisciplinary Journal of Nonlinear Science
language:en
Short-container-title:Chaos

Author:

Kasthuri Praveen¹,Pavithran Induja²,Pawar Samadhan A.¹^ORCID,Sujith R. I.¹^ORCID,Gejji Rohan³^ORCID,Anderson William³^ORCID

Affiliation:

1. Department of Aerospace Engineering, Indian Institute of Technology, IIT Madras, Chennai 600036, India

2. Department of Physics, Indian Institute of Technology, IIT Madras, Chennai 600036, India

3. School of Aeronautics and Astronautics, Purdue University, West Lafayette, Indiana 47907, USA

Funder

Air Force Office of Scientific Research

Publisher

AIP Publishing

Subject

Applied Mathematics,General Physics and Astronomy,Mathematical Physics,Statistical and Nonlinear Physics

Link

http://aip.scitation.org/doi/am-pdf/10.1063/1.5120429

Reference67 articles.

1. THE EXPLANATION OF CERTAIN ACOUSTICAL PHENOMENA 1

2. Effect of Wave Propagation in Feed Lines on Low-Frequency Rocket Instability

3. Longitudinal instability of liquid rockets due to propulsion feedback /POGO/.

4. Nozzle Damping in Solid Rocket Instabilities

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2. Detached eddy simulation of the interaction between acoustics and flame dynamics during the transition before and after longitudinal thermoacoustic instability in a multi-element liquid rocket engine;Physics of Fluids;2024-06-01

3. Thermoacoustic velocity and pressure oscillations in one-dimensional combustors with spatially varying heat sources and thermal distributions;Physics of Fluids;2024-04-01

4. Early detection of thermoacoustic instability in an O2/CH4 single-injector rocket combustor using analysis of chaos and deep learning models;Physics of Fluids;2024-03-01

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