NASA Logo

NTRS

NTRS - NASA Technical Reports Server

Back to Results
Investigation of the Flow-Induced Vibration in the E2 Test FacilityAn investigation of flow induced vibration due to coupling between the fluid flow and the propellants lines (LOX and RP-1) was performed. Various flow rate conditions were studied to check whether flow induced vibration was possible due to vortex shedding in both valves and pipe lines. Resonance test was conducted for all segments of the LOX-feedline for the preburner under test. In addition, critical values of frequency and velocity are calculated using a mass damping model. A simple chart characterizing the relation between frequency and velocity is developed for each component; i.e. propellant lines, valves and flow meters. It was found that flow induced vibration occurs for various segments with flow rates of 113 lb/s, 275 lb/s and 40 lb/s. Even more interesting using critical conditions for buckling, it was found that the valve or pipe may collapse for a flow rate of 275 lb/s and valve height of 10% of pipe diameter. Furthermore, two models for the acoustic pressure acting on the segments particularly for the valve are proposed.
Document ID
20040040336
Acquisition Source
Stennis Space Center
Document Type
Other - NASA Publication (NP)
Authors
Castillo, Luciano
(Rensselaer Polytechnic Inst. Troy, NY, United States)
Date Acquired
September 7, 2013
Publication Date
August 17, 2001
Subject Category
Fluid Mechanics And Thermodynamics
Report/Patent Number
NASA/NP-2002-02-00006-SSC
Distribution Limits
Public
Copyright
Work of the US Gov. Public Use Permitted.
No Preview Available