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Analyses Of Transient Events In Complex Valve and Feed SystemsValve systems in rocket propulsion systems and testing facilities are constantly subject to dynamic events resulting from the timing of valve motion leading to unsteady fluctuations in pressure and mass flow. Such events can also be accompanied by cavitation, resonance, system vibration leading to catastrophic failure. High-fidelity dynamic computational simulations of valve operation can yield important information of valve response to varying flow conditions. Prediction of transient behavior related to valve motion can serve as guidelines for valve scheduling, which is of crucial importance in engine operation and testing. In this paper, we present simulations of the diverse unsteady phenomena related to valve and feed systems that include valve stall, valve timing studies as well as cavitation instabilities in components utilized in the test loop.
Document ID
20050201913
Acquisition Source
Stennis Space Center
Document Type
Preprint (Draft being sent to journal)
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)
Cavallo, Peter
(Combustion Research and Flow Technology, Inc. Pipersville, PA, United States)
Daines, Russell
(Jacobs Sverdrup Technology, Inc. Huntsville, AL, United States)
Date Acquired
August 23, 2013
Publication Date
January 1, 2005
Subject Category
Spacecraft Propulsion And Power
Report/Patent Number
NASA/NP-2005-06-00064-SSC
Meeting Information
Meeting: 41st AIAA/ASME/SAE/ASEE Joint Propulsion Conference and Exhibit
Location: Tucson, AZ
Country: United States
Start Date: July 10, 2005
End Date: July 13, 2005
Sponsors: American Inst. of Aeronautics and Astronautics, Society of Automotive Engineers, Inc., American Society for Electrical Engineers, American Society of Mechanical Engineers
Funding Number(s)
CONTRACT_GRANT: NNS04AA08C
Distribution Limits
Public
Copyright
Public Use Permitted.
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