Akhil Aravind

Akhil Aravind
  • Master of Technology
  • PhD Student at Indian Institute of Science Bangalore

PhD Student

About

15
Publications
729
Reads
How we measure 'reads'
A 'read' is counted each time someone views a publication summary (such as the title, abstract, and list of authors), clicks on a figure, or views or downloads the full-text. Learn more
15
Citations
Current institution
Indian Institute of Science Bangalore
Current position
  • PhD Student
Education
August 2021 - December 2025
Indian Institute of Science Bangalore
Field of study
  • Mechanical Engineeirng
June 2019 - April 2021
Indian Institute of Technology Kanpur
Field of study
  • Aerospace Engineering
June 2015 - April 2019
R.V. College of Engineering
Field of study
  • Mechanical Engineering

Publications

Publications (15)
Article
Understanding the dynamics of flames at small scales opens up opportunities to enhance the performance of small-scale power generation devices, micro-reactors, fire safety devices and numerous other systems that confine combustion to micro/meso scales. The current study investigates the dynamics of laminar premixed methane–air flames in meso-scale...
Conference Paper
Full-text available
Liquid interfaces interacting with high-speed gas flows result in unsteady waves, atomization and countless applications. Here, we capture the intricate dynamics of a blast-induced air flow interacting with a liquid jet at the opening of a shock tube with a rectangular cross-section (aspect ratio 2:1). Features like a blast wave and the induced air...
Article
This study comprehensively investigates the response of a combusting droplet during its interaction with a high-speed transient flow imposed by a coaxially propagating blast wave. The blast wave is generated using a specially designed miniature shock generator that produces blast waves using the wire-explosion technique, facilitating a wide range o...
Preprint
The study comprehensively investigates the response of a combusting droplet during its interaction with high-speed transient flow imposed by a coaxially propagating blast wave. The blast wave is generated using a miniature shock generator which facilitates wide Mach number range ($1.01<M_s<1.6$). The interaction of the shock flow occurs in two stag...
Article
The present study investigates the flame dynamics of a contactless burning fuel droplet under free fall subjected to a co-flow. The dynamic external relative flow established due to co-flow and droplet acceleration results in a series of droplet flame transitions. Different flame structures were observed, including a wake flame, reversed wake flame...
Preprint
The study investigates the response of non-premixed jet flames to blast waves that are incident along the jet axis in the direction of the fuel jet. The flame is found to exhibit two major response patterns: re-attachment and extinction. Reducing the fuel jet Reynolds number (Re) and increasing the interacting blast wave Mach numbers (Ms) were foun...
Preprint
The study investigates the response of the premixed jet flame during its interaction with the coaxial blast wave incident towards the flame. The blast wave is generated using a unique miniature shock generation facility that employs the wire-explosion technique, which enables a fine and easier control of the strength of the shock waves generated (M...
Preprint
Understanding the dynamics of flames at small scales opens up opportunities to enhance the performance of small-scale power generation devices (which have potential appliances in micro-electro-mechanical systems), micro-reactors (which are extensively used in the field of quantitative chemistry), fire safety devices, and numerous other systems that...
Article
Airfoils pitching in the stalled regime have been of keen interest in recent years due to their desirable aerodynamic force characteristics. This study numerically investigates the unsteady flow past a NACA (National Advisory Committee for Aeronautics) 0012 airfoil under sinusoidally pitching motion using a sharp interface immersed boundary framewo...
Preprint
Full-text available
Airfoils pitching in the stalled regime have been of keen interest in recent years due to their desirable aerodynamic force characteristics. In this study, we are numerically investigating the unsteady flow past a NACA 0012 airfoil under sinusoidally pitching motion, using a finite volume based sharp interface immersed boundary solver. The flow is...

Network

Cited By