KHz-rate velocity measurements using pulse-burst, cross-correlation Doppler global velocimetry

Abstract Pulse-burst, cross-correlation Doppler global velocimetry was used to perform kHz-rate velocity measurements in the NASA Langley 4-Foot Supersonic Unitary Plan Wind Tunnel. Planar, one component (2D-1C) velocity measurements were made at rates up to 6 kHz in a canonical, oblique shockwave flowfield, generated by a full-span splitter plate in a Mach 2.4 flow. Assessment of the velocimetric accuracy indicates agreement with theoretical velocity values to within 1-percent on average for all measurements tested. The spatial velocity precision is measured to be between 0.3 and 0.5% (1 <mml:math xmlns:mml="http://www.w3.org/1998/Math/MathML" overflow="scroll"> <mml:mrow> <mml:mi>σ</mml:mi> </mml:mrow> </mml:math> ) for all tested frequencies, while the ensemble (1 σ ) precision of the measurements was within 2.3% of the measured velocities. Measurement uncertainties that were estimated using Monte Carlo simulations exhibit values similar to the precision (2%) and also indicate the potential for biases in the velocity results as a result of periodic or modal behavior in flows. While these results are promising, the technique also shows great potential for expansion, both in measurement rates and applicability to other techniques.

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Publication Details

Journal
Measurement Science and Technology
Published
2025-04-22
DOI
https://doi.org/10.1088/1361-6501/adcf3c
Primary Topic
Spectroscopy and Laser Applications
Type
article
Field-Weighted Citation Impact
0.00

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article

KHz-rate velocity measurements using pulse-burst, cross-correlation Doppler global velocimetry

Timothy W. Fahringer, Ross A. Burns, Paul M. Danehy
Measurement Science and Technology
Spectroscopy and Laser Applications
article

KHz-rate velocity measurements using pulse-burst, cross-correlation Doppler global velocimetry

Timothy W. Fahringer, Ross A. Burns, Paul M. Danehy
article en

Abstract

Abstract Pulse-burst, cross-correlation Doppler global velocimetry was used to perform kHz-rate velocity measurements in the NASA Langley 4-Foot Supersonic Unitary Plan Wind Tunnel. Planar, one component (2D-1C) velocity measurements were made at rates up to 6 kHz in a canonical, oblique shockwave flowfield, generated by a full-span splitter plate in a Mach 2.4 flow. Assessment of the velocimetric accuracy indicates agreement with theoretical velocity values to within 1-percent on average for all measurements tested. The spatial velocity precision is measured to be between 0.3 and 0.5% (1 <mml:math xmlns:mml="http://www.w3.org/1998/Math/MathML" overflow="scroll"> <mml:mrow> <mml:mi>σ</mml:mi> </mml:mrow> </mml:math> ) for all tested frequencies, while the ensemble (1 σ ) precision of the measurements was within 2.3% of the measured velocities. Measurement uncertainties that were estimated using Monte Carlo simulations exhibit values similar to the precision (2%) and also indicate the potential for biases in the velocity results as a result of periodic or modal behavior in flows. While these results are promising, the technique also shows great potential for expansion, both in measurement rates and applicability to other techniques.

Measurement Science and TechnologyVol. 36(5)
Langley Research Center (US), ViGYAN (United States) (US)
National Aeronautics and Space Administration
Openalex Percentile: Top 92%
Spectroscopy and Laser Applications
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