Experimental Investigation of Spray Dynamics in Cross-flowing air at high Weber number-Reference-Cited by-同舟云学术

Experimental Investigation of Spray Dynamics in Cross-flowing air at high Weber number

Published:2006-07-09 Issue: Volume: Page:
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Container-title:42nd AIAA/ASME/SAE/ASEE Joint Propulsion Conference & Exhibit
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Author:

Gopala Yogish,Lubarsky Eugene,Bibik O.,Zinn Ben,Dai Zhongtao

Publisher

American Institute of Aeronautics and Astronautics

Reference14 articles.

2. 2Bonnell, J. M., Marchall, R. L., and Riecke, G. T. "Combustion Instability in turbojet and Turbofan Augmentors", AIAA 71-698,7th AIAA/SAE Propulsion Joint Specialist Conference Exhibit, Salt Lake City, UT 1971.

3. 4Tambe, S. B., Jeng, S. M., Mongia, H., and Hsiao, G. "Liquid Jets in Subsonic Flow", AIAA 2005-731,43st AerospaceScience Meeting &Exhibit, Reno,NV2005.

4. 6Wu, P.K., Hsiang, L.P., and Faeth, G. M. ``Aerodynamic Effects on Primary and Secondary Breakup,'' Liquid Rocket Engine Combustion Instability, edited by V. Yang and W. Anderson, Vol.169, Progress in Astronautics andAeronautics, AIAA,Washington,DC,1995,pp.247-279.

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