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The Effect of Resistance on Rocket Injector AcousticsCombustion instability, where unsteady heat release couples with acoustic modes, has long been an area of concern in liquid rocket engines. Accurate modeling of the acoustic normal modes of the combustion chamber is important to understanding and preventing combustion instability. The injector resistance can have a significant influence on the chamber normal mode shape, and hence on the system stability.
Document ID
20150021468
Acquisition Source
Marshall Space Flight Center
Document Type
Presentation
Authors
Morgan, C. J.
(Jacobs Engineering and Science Services and Skills Augmentation Group (ESSSA) Huntsville, AL, United States)
Date Acquired
November 19, 2015
Publication Date
October 7, 2015
Subject Category
Numerical Analysis
Fluid Mechanics And Thermodynamics
Report/Patent Number
M15-4868
Report Number: M15-4868
Meeting Information
Meeting: COMSOL Conference 2015
Location: Boston, MA
Country: United States
Start Date: October 7, 2015
End Date: October 9, 2015
Sponsors: COMSOL, Inc.
Funding Number(s)
CONTRACT_GRANT: NNM12AA41C
Distribution Limits
Public
Copyright
Public Use Permitted.
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