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Dive into the research topics where Yedhu Krishna is active.

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Featured researches published by Yedhu Krishna.


Applied Optics | 2014

Baseline correction for stray light in log-ratio diode laser absorption measurements.

Yedhu Krishna; Sean O’Byrne; Joe Kurtz

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 is difficult to avoid stray light falling on the signal photodiode of the sensor. This stray light acts as noncommon-mode interference and introduces a systematic error in absorption measurements, which is not removed by baseline subtraction. This paper analyzes the factors that determine this systematic error and also presents a calibration method that can correct for it. This correction method is verified using a simple experiment.


53rd AIAA Aerospace Sciences Meeting | 2015

Flight test of a rugged scramjet-inlet temperature and velocity sensor

Joe Kurtz; Mark Aizengendler; Yedhu Krishna; Paul Walsh; Sean O'Byrne

The performance of a gas temperature and velocity sensor based on tuneable diode laser absorption spectroscopy (TDLAS) of oxygen in a scramjet engine inlet during a flight test is discussed. This is the first flight-tested TDLAS sensor designed specifically for measuring gas velocity of a scramjet inlet flow under flight conditions. The robustness and stability of the sensor design in dynamic load conditions were made evident by the quality of the data delivered after a very unstable and high-g launch scenario. The scramjet did not reach the targeted test altitude-velocity regime. However, analysis of the low-altitude data determined pressure and temperature in the inlet and showed that an adequate signal-to-noise ratio was obtained for high-speed velocity measurements at altitudes up to at least 30 km.


International Symposium on Shock Waves | 2013

Diode-Laser-Based Driver Gas Detector for Hypersonic Shock Tunnels

Yedhu Krishna; Sean O’Byrne; Mark Aizengendler

Measurement of the useful flow duration in ground-based hypersonic flow facilities, especially for impulse facilities which have relatively short output flow duration, poses significant measurement challenges.


Optics and Lasers in Engineering | 2010

Engineering the size of dark core of an optical vortex

Ashok Kumar; Pravin Vaity; Yedhu Krishna; R. P. Singh


Journal of Propulsion and Power | 2015

Numerically Determining Mach Number and Orientation in Hypersonic Inlets Using Absorption Spectroscopy

Yedhu Krishna; Sean O’Byrne; Sven Wittig; Joe Kurtz


31st AIAA Aerodynamic Measurement Technology and Ground Testing Conference | 2015

A Time-Resolved Temperature Measurement System for Free-Piston Shock Tunnels

Yedhu Krishna; Suzanne L. Sheehe; Sean O'Byrne


AIAA Journal | 2016

Rugged, Scramjet Inlet Temperature and Velocity Sensor: Design and Ground Test

Joe Kurtz; Mark Aizengendler; Yedhu Krishna; Paul Walsh; Sean O’Byrne


Archive | 2013

A Rugged, High-Sensitivity, TDLAS-based Oxygen Sensor for a Scramjet Inlet

Mark Aizengendler; Yedhu Krishna; Joe Kurtz; Sean O'Byrne; Paul Walsh


AIAA Journal | 2016

Subsonic In-Flight Temperature and Pressure Measurements Using a Scramjet Inlet Flow Sensor

Joe Kurtz; Mark Aizengendler; Yedhu Krishna; Paul Walsh; Melrose Brown; Sean O’Byrne


Australian Space Science Conference 2011. | 2011

Diode Laser Measurement of Mach Number and Angle of Attack in a Hypersonic Inlet

Yedhu Krishna; Joe Kurtz; Sean O'Byrne

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Joe Kurtz

University of Arizona

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Mark Aizengendler

University of New South Wales

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Sean O'Byrne

University of New South Wales

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Sean O’Byrne

University of New South Wales

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Suzanne L. Sheehe

University of New South Wales

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Andrew J. Neely

University of New South Wales

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Harald Kleine

University of New South Wales

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S. L. Gai

University of New South Wales

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Ashok Kumar

Physical Research Laboratory

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