Fast Acting Probe for Measurement of Turbulent Pressure and Temperature Fluctuations in a Gas Turbine Combustor-Reference-Cited by-同舟云学术

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Fast Acting Probe for Measurement of Turbulent Pressure and Temperature Fluctuations in a Gas Turbine Combustor

Published:2006-01-09 Issue: Volume: Page:
ISSN:
Container-title:44th AIAA Aerospace Sciences Meeting and Exhibit
language:
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Author:

Passaro Andrea¹,Biagioni Leonardo¹,LaGraff John²,Oldfield Martin³

Affiliation:

1. Alta SpA

2. Syracuse University

3. Oxford University

Publisher

American Institute of Aeronautics and Astronautics

Link

http://arc.aiaa.org/doi/pdf/10.2514/6.2006-550

Reference20 articles.

1. Simultaneous coherent anti-Stokes Raman spectroscopy measurements inhydrogen-fueled supersonic combustion

2. Measurement of energy spectra in weakly compressible turbulence

3. Buttsworth, D.R. and Jones, T.V. "A Fast-Response Total Temperature Probe for Unsteady Compressible Flows", ASME Paper96-GT-350,1996.

Cited by 3 articles. 订阅此论文施引文献订阅此论文施引文献，注册后可以免费订阅5篇论文的施引文献，订阅后可以查看论文全部施引文献

1. Acoustic wave propagation in a sensor port: Experimental measurements and analytical model predictions;Applied Acoustics;2017-12

2. A High Temperature High Bandwidth Fast Response Total Pressure Probe for Measurements in a Multistage Axial Compressor;Journal of Engineering for Gas Turbines and Power;2012-04-12

3. A Conceptual Design Study for a New High Temperature Fast Response Cooled Total Pressure Probe;Journal of Engineering for Gas Turbines and Power;2008-12-29

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