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Uncertainty Analysis of Experimental Discharge Coefficients in Additively Manufactured Liquid Injector ElementsScreening of two additively manufactured liquid injector designs was conducted in the UAH high pressure spray facility. Four variants of each geometry with slightly different dimensions were obtained from eleven separate commercial additive manufacturing services. The devices were manufactured from Inconel 625 using the selective laser melting (SLM) powder bed process. The devices were cold flowed with water over a range of relevant pressure drops (75 psi to 1500 psi) to produce water flow rates from 0.037 to 1.75 lbm/s into ambient back pressure. Discharge coefficients determined from the testing along with the associated uncertainties provide insight into characteristic flow performance variabilities that can be expected from the SLM process for similar geometries.
Document ID
20190030431
Acquisition Source
Marshall Space Flight Center
Document Type
Conference Paper
Authors
Venters, James P.
(Alabama Univ. Huntsville, AL, United States)
Costa, Melissa
(Alabama Univ. Huntsville, AL, United States)
Unruh, Evan C.
(Alabama Univ. Huntsville, AL, United States)
Lineberry, David M.
(Alabama Univ. Huntsville, AL, United States)
Frederick, Robert A.
(Alabama Univ. Huntsville, AL, United States)
Wood, Jessica
(NASA Marshall Space Flight Center Huntsville, AL, United States)
Hulka, James
(Jacobs Engineering Group Huntsville, AL, United States)
Date Acquired
September 4, 2019
Publication Date
August 19, 2019
Subject Category
Spacecraft Propulsion And Power
Report/Patent Number
M19-7538
Report Number: M19-7538
Meeting Information
Meeting: AIAA Propulsion and Energy Forum and Exposition
Location: Indianapolis, IN
Country: United States
Start Date: August 19, 2019
End Date: August 22, 2019
Sponsors: American Institute of Aeronautics and Astronautics (AIAA)
Distribution Limits
Public
Copyright
Public Use Permitted.
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