Quantifying the Variation of the Mass Flow Rate Generated in a Simplex Swirl Injector by Pressure Fluctuation-Reference-Cited by-同舟云学术

Quantifying the Variation of the Mass Flow Rate Generated in a Simplex Swirl Injector by Pressure Fluctuation

Published:2008-07-21 Issue: Volume: Page:
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Container-title:44th AIAA/ASME/SAE/ASEE Joint Propulsion Conference & Exhibit
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Author:

Khil Taeock,Kim Sunghyuk,Cho Seongho,Yoon Youngbin

Publisher

American Institute of Aeronautics and Astronautics

Reference17 articles.

1. 1Culick, F.E.C. and Yang, V. "Overview of Combustion Instability in Liquid-Propellant RocketEngine," AIAA Conference in Astronauticsand Aeronautics, Vol.169, 1995, pp3-38.

2. 3Rubinsky, V.R. "Combustion Instability in the RD-0110 Engine," AIAA Conference in Astronautics and Aeronautics, Vol 169, 1995, pp89-112.

3. Liquid-Propellant Rocket Engine Injector Dynamics

4. 6Bazarov, V., Lee, E., Lineberry, D., Swanner, B., and Frederick, A. Jr. "Pulsator Designs for Liquid Rocket Injector Research,"43rdAIAA/ASME/SAE/ASEE Joint PropulsionConference &Exhibit,Cincinnatim, OH, July. 8-11,2007.

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