CARS thermometry in a supersonic combustor for CFD code validation-Reference-Cited by-同舟云学术

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CARS thermometry in a supersonic combustor for CFD code validation

Published:2002-01-14 Issue: Volume: Page:
ISSN:
Container-title:40th AIAA Aerospace Sciences Meeting & Exhibit
language:
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Author:

Cutler A.¹,Danehy P.,Springer R.,DeLoach R.,Capriotti D.

Affiliation:

1. NASA, Langley Research Center, Hampton, VA

Publisher

American Institute of Aeronautics and Astronautics

Link

http://arc.aiaa.org/doi/pdf/10.2514/6.2002-743

Cited by 9 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. Conjugate Heat Transfer Analysis of Scramjet Combustor;Journal of Aerospace Sciences and Technologies;2023-08-01

2. Air volume flow rate optimization of the guide vanes in an axial flow fan based on DOE and CFD;Scientific Reports;2023-03-17

3. Wall Roughness Effects on Combustion Development in Confined Supersonic Flow;Journal of Propulsion and Power;2021-01

4. Using Modern Design of Experiments to Create a Surface Pressure Database From a Low Speed Wind Tunnel Test;24th AIAA Aerodynamic Measurement Technology and Ground Testing Conference;2004-06-19

5. Dual-Pump CARS Thermometry and Species Concentration Measurements in a Supersonic Combustor;42nd AIAA Aerospace Sciences Meeting and Exhibit;2004-01-05

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