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Simulations of Instabilities in Complex Valve and Feed SystemsCFD analyses are playing an increasingly important role in identifying and characterizing flow induced instabilities in rocket engine test facilities and flight systems. In this paper, we analyze instability mechanisms that range from turbulent pressure fluctuations due to vortex shedding in structurally complex valve systems to flow resonance in plug cavities to large scale pressure fluctuations due to collapse of cavitation induced vapor clouds. Furthermore, we discuss simulations of transient behavior related to valve motion that can serve as guidelines for valve scheduling. Such predictions of valve response to varying flow conditions is of crucial importance to engine operation and testing.
Document ID
20070018857
Acquisition Source
Stennis Space Center
Document Type
Conference Paper
Authors
Ahuja, Vineet
(Combustion Research and Flow Technology, Inc. Pipersville, PA, United States)
Hosangadi, Ashvin
(Combustion Research and Flow Technology, Inc. Pipersville, PA, United States)
Shipman, Jeremy
(Combustion Research and Flow Technology, Inc. Pipersville, PA, United States)
Cavallo, Peter A.
(Combustion Research and Flow Technology, Inc. Pipersville, PA, United States)
Date Acquired
August 23, 2013
Publication Date
January 1, 2006
Subject Category
Fluid Mechanics And Thermodynamics
Report/Patent Number
AIAA Paper 2006-4758
SSTI-8080-0009
Report Number: AIAA Paper 2006-4758
Report Number: SSTI-8080-0009
Meeting Information
Meeting: 42nd AIAA/ASME/SAE/ASEE Joint Propulsion Conference & Exhibit
Location: Sacramento, CA
Country: United States
Start Date: July 9, 2006
End Date: July 12, 2006
Sponsors: American Society for Electrical Engineers, Society of Automotive Engineers, Inc., American Inst. of Aeronautics and Astronautics, American Society of Mechanical Engineers
Funding Number(s)
CONTRACT_GRANT: NNS05AA36C
CONTRACT_GRANT: NNS04AA08C
CONTRACT_GRANT: NNS05AA08P
Distribution Limits
Public
Copyright
Public Use Permitted.
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