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NO PLIF imaging in the CUBRC 48-inch shock tunnel
Nitric oxide planar laser-induced fluorescence (NO PLIF) imaging is demonstrated at a 10-kHz repetition rate in the Calspan University at Buffalo Research Center’s (CUBRC) 48-inch Mach 9 hypervelocity shock tunnel using a pulse burst laser–based high frame rate imaging system. Sequences of up to ten...
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| Published in: | Experiments in fluids 2012-12, Vol.53 (6), p.1637-1646 |
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| Main Authors: | , , , , , , , , , , , , |
| Format: | Article |
| Language: | English |
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| cited_by | cdi_FETCH-LOGICAL-c427t-e71793a42797b8f07966053a8b19055002d99694fa97c8a7dc19fc69a4984513 |
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| cites | cdi_FETCH-LOGICAL-c427t-e71793a42797b8f07966053a8b19055002d99694fa97c8a7dc19fc69a4984513 |
| container_end_page | 1646 |
| container_issue | 6 |
| container_start_page | 1637 |
| container_title | Experiments in fluids |
| container_volume | 53 |
| creator | Jiang, N. Bruzzese, J. Patton, R. Sutton, J. Yentsch, R. Gaitonde, D. V. Lempert, W. R. Miller, J. D. Meyer, T. R. Parker, R. Wadham, T. Holden, M. Danehy, P. M. |
| description | Nitric oxide planar laser-induced fluorescence (NO PLIF) imaging is demonstrated at a 10-kHz repetition rate in the Calspan University at Buffalo Research Center’s (CUBRC) 48-inch Mach 9 hypervelocity shock tunnel using a pulse burst laser–based high frame rate imaging system. Sequences of up to ten images are obtained internal to a supersonic combustor model, located within the shock tunnel, during a single ~10-millisecond duration run of the ground test facility. Comparison with a CFD simulation shows good overall qualitative agreement in the jet penetration and spreading observed with an average of forty individual PLIF images obtained during several facility runs. |
| doi_str_mv | 10.1007/s00348-012-1381-6 |
| format | article |
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Thermal use of fuels</subject><subject>Engineering</subject><subject>Engineering Fluid Dynamics</subject><subject>Engineering Thermodynamics</subject><subject>Engines and turbines</subject><subject>Equipments for energy generation and conversion: thermal, electrical, mechanical energy, etc</subject><subject>Exact sciences and technology</subject><subject>Fluid dynamics</subject><subject>Fluid flow</subject><subject>Fluid- and Aerodynamics</subject><subject>Fluids</subject><subject>Fundamental areas of phenomenology (including applications)</subject><subject>Heat and Mass Transfer</subject><subject>Imaging</subject><subject>Instrumentation for fluid dynamics</subject><subject>Physics</subject><subject>Research Article</subject><subject>Shock tunnels</subject><subject>Spreading</subject><issn>0723-4864</issn><issn>1432-1114</issn><fulltext>true</fulltext><rsrctype>article</rsrctype><creationdate>2012</creationdate><recordtype>article</recordtype><recordid>eNqFkE1PwzAMhiMEEmPwA7j1gsSlYCdpPo5QMZg0MYTGOcqydOvo0tF0B_49mTZxhJNt-fEr-SHkGuEOAeR9BGBc5YA0R6YwFydkgJylCZGfkgFIynKuBD8nFzGuAbDQoAYEX6fZ22Q8yuqNXdZhmdUh61c-Kz8e38ssJdbBrbK4at1n1u9C8M0lOatsE_3VsQ7JbPQ0K1_yyfR5XD5Mcsep7HMvUWpmU6_lXFUgtRBQMKvmqKEoAOhCa6F5ZbV0ysqFQ105oS3XihfIhuT2ELvt2q-dj73Z1NH5prHBt7toUHBKVULV_2iBlFEsgCcUD6jr2hg7X5ltlz7vvg2C2Ys0B5EmiTR7kUakm5tjvI3ONlVng6vj7yEVQnHGi8TRAxfTKix9Z9btrgvJ0R_hP3FbfSE</recordid><startdate>20121201</startdate><enddate>20121201</enddate><creator>Jiang, N.</creator><creator>Bruzzese, J.</creator><creator>Patton, R.</creator><creator>Sutton, J.</creator><creator>Yentsch, R.</creator><creator>Gaitonde, D. 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| ispartof | Experiments in fluids, 2012-12, Vol.53 (6), p.1637-1646 |
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| subjects | Applied sciences Bursting Computational fluid dynamics Energy Energy. Thermal use of fuels Engineering Engineering Fluid Dynamics Engineering Thermodynamics Engines and turbines Equipments for energy generation and conversion: thermal, electrical, mechanical energy, etc Exact sciences and technology Fluid dynamics Fluid flow Fluid- and Aerodynamics Fluids Fundamental areas of phenomenology (including applications) Heat and Mass Transfer Imaging Instrumentation for fluid dynamics Physics Research Article Shock tunnels Spreading |
| title | NO PLIF imaging in the CUBRC 48-inch shock tunnel |
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