Yedhu Krishna

ORCID: 0000-0003-1440-0171
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About
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Research Areas
  • Spectroscopy and Laser Applications
  • Combustion and flame dynamics
  • Advanced Combustion Engine Technologies
  • Atmospheric Ozone and Climate
  • Gas Dynamics and Kinetic Theory
  • Atmospheric and Environmental Gas Dynamics
  • Advanced Sensor Technologies Research
  • Radiative Heat Transfer Studies
  • Fluid Dynamics and Turbulent Flows
  • Laser Design and Applications
  • Particle Dynamics in Fluid Flows
  • Photonic and Optical Devices
  • Ionosphere and magnetosphere dynamics
  • Fluid Dynamics and Heat Transfer
  • Advanced Optical Sensing Technologies
  • Combustion and Detonation Processes
  • Plasma Diagnostics and Applications
  • Aerodynamics and Acoustics in Jet Flows
  • Plasma and Flow Control in Aerodynamics
  • Plant Surface Properties and Treatments
  • Calibration and Measurement Techniques
  • Advanced Photonic Communication Systems
  • Computational Fluid Dynamics and Aerodynamics
  • Rocket and propulsion systems research
  • Spectroscopy Techniques in Biomedical and Chemical Research

King Abdullah University of Science and Technology
2018-2023

Indian Institute of Space Science and Technology
2023

Indian Institute of Science Bangalore
2010-2021

University of Canberra
2014-2018

UNSW Sydney
2014-2018

ACT Government
2015-2018

Australian Defence Force Academy
2015

Cochin University of Science and Technology
2009

Physical Research Laboratory
2009

Abstract The non-invasive nature of optical diagnostic techniques is advantageous in studying micronozzles, as it safeguards the undisturbed highly sensitive micro-scale flow field. In this work, a laser-based interferometric Mie scattering system developed using virtually imaged phased array to quantitatively measure one-dimensional velocity profile at exit micronozzles. A narrow-linewidth solid-state laser used light source, acetone-seeded air gas, and estimated from Doppler shift...

10.1088/1361-6501/adc149 article EN Measurement Science and Technology 2025-03-17

10.1016/j.optlaseng.2009.11.009 article EN Optics and Lasers in Engineering 2009-12-16

The design and testing of a gas temperature velocity scramjet engine inlet sensor based on tunable diode laser absorption spectroscopy oxygen is discussed. robustness stability the optical necessitated by dynamic vibrational thermal environment were balanced against need for compact size very high signal-to-noise ratio in low-pressure, high-altitude flight regime. Test results demonstrated good mechanical an adequate altitudes up to 30 km with predicted absorbance peaks greater than signal...

10.2514/1.j054303 article EN AIAA Journal 2015-07-29

A 10-kHz one-dimensional Rayleigh-CH4 Raman instrument capable of achieving highly precise measurement temperature and methane mole fraction is demonstrated. The system uses a pulse-burst laser as the light source back-illuminated electron-multiplied CCD cameras detectors. are operated in subframe burst gating mode, to combine high sampling rate, low noise, slow readout. improved precision this configuration demonstrated by measuring fractions ambient gas mixtures non-premixed inverse...

10.1364/ol.44.004091 article EN Optics Letters 2019-08-20

A numerical method is presented for measuring angle of attack and Mach number in the inlet a supersonic combustor using sensor design based on tunable diode laser absorption spectroscopy. nonlinear least-squares fitting routine was applied to simultaneously retrieve freestream simple two-dimensional with known conical simulated spectrum. The spectrum spanned over five transitions -band molecular oxygen. In presence 15% white Gaussian background noise, converged actual value standard...

10.2514/1.b35187 article EN Journal of Propulsion and Power 2014-04-21

The work introduces a VIPA-based interferometric Rayleigh scattering instrument for tracer-free, simultaneous temperature and velocity measurements along 1D volume. A virtually imaged phased array (VIPA) replaces the Fabry-Perot etalon conventionally used in scattering, allowing extension of technique from 0D (point or multi-point) to 1D. Rayleigh-Brillouin spectrum is function pressure can be diagnostics isobaric flows. reference leg based on (FP) provides real-time monitoring laser...

10.1364/oe.524049 article EN cc-by Optics Express 2024-05-08

The two-color ratio pyrometry technique using a digital single-lens reflex camera has been used to measure the time-averaged and path-integrated temperature distribution in radiating shock layer high-enthalpy flow. A 70 mm diameter cylindrical body with long spike was placed hypersonic tunnel, region behind investigated. systematic error due contributions from line emissions corrected by monitoring emission spectrum this spectrometer. relative on R, G, B channels of were 7.4%, 2.2%, 0.4%,...

10.1364/ao.56.008492 article EN Applied Optics 2017-10-17

Log-ratio detection is a convenient technique for making temperature and concentration measurements using sensors based on tunable diode laser absorption spectroscopy. In many practical sensing applications, it difficult to avoid stray light falling the signal photodiode of sensor. This acts as noncommon-mode interference introduces systematic error in measurements, which not removed by baseline subtraction. paper analyzes factors that determine this also presents calibration method can...

10.1364/ao.53.004128 article EN Applied Optics 2014-06-20

The performance of a scramjet inlet sensor based on tunable diode laser absorption spectroscopy oxygen in the A-band near 760 nm during low-altitude, subsonic flight test is discussed. Though did not reach targeted hypersonic regime due to malfunction first-stage booster, analysis spectral data acquired descent below 3 km successfully determined pressure and temperature demonstrated that system was capable producing an adequate signal-to-noise ratio allow temperature, pressure, velocity...

10.2514/1.j054207 article EN AIAA Journal 2015-12-23

The performance of a gas temperature and velocity sensor based on tuneable diode laser absorption spectroscopy (TDLAS) oxygen in scramjet engine inlet during flight test is discussed. This the first flight-tested TDLAS designed specifically for measuring flow under conditions. robustness stability design dynamic load conditions were made evident by quality data delivered after very unstable high-g launch scenario. did not reach targeted altitude-velocity regime. However, analysis...

10.2514/6.2015-0110 article EN 53rd AIAA Aerospace Sciences Meeting 2015-01-03

One-dimensional interferometric Rayleigh scattering velocimetry is demonstrated using a virtually imaged phased array (VIPA). A continuous-wave laser emitting at 532 nm used as the source, and low-noise CCD camera detector. The VIPA has free spectral range of 15 GHz coated for wavelength 500-600 nm. Velocity measurements different flow rates show an accuracy 10 m/s. Demonstration high-speed velocity measurement conducted in jet air through contoured converging nozzle. Factors considered...

10.1364/ol.441913 article EN Optics Letters 2021-09-28

A filtered Rayleigh scattering system is developed and applied to measure the mole fraction of methane in a methane-air swirl flow through transparent conical quartz quarl. Light from location where laser beam incident on surface quarl orders magnitudes larger than gas mixture interest. This diffusive suppressed using molecular absorption by an iodine cell spatial filtering optical aperture. Residual stray light accounted for up 5% total signal had be removed accurate measurements. The...

10.1364/ao.58.005575 article EN Applied Optics 2019-07-09

This paper presents a comprehensive study on the design and performance evaluation of circular rectangular microstrip patch antennas tailored for 5G applications, operating at 25 GHz. Utilizing Teflon Rogers substrates with superior dielectric properties, are meticulously crafted rigorously analyzed. The explores methodology, simulation outcomes, compares antennas, focusing their suitability systems. Through iterative simulations optimizations, fine-tuned to achieve optimal parameters,...

10.46610/jaeed.2024.v02i02.002 article EN Journal of Advance Electrical Engineering and Devices 2024-01-01

A method for measuring the velocity of liquid droplets emanating from an effervescent injector into ambient air was experimented using a mixture acetone and water. Conventional methods such as Laser Doppler Velocimetry Particle Image Velocimetry, which utilise Mie-scattering, have limitations due to multiple scattering strong surface reflections, respectively. In current study, we demonstrate fluorescence-based particle image velocimetry, can overcome abovementioned difficulty. Unlike...

10.55037/lxlaser.21st.184 article EN 2024-07-08
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