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Computer Modeling of Direct Metal Laser SinteringA computational approach to modeling direct metal laser sintering (DMLS) additive manufacturing process is presented. The primary application of the model is for determining the temperature history of parts fabricated using DMLS to evaluate residual stresses found in finished pieces and to assess manufacturing process strategies to reduce part slumping. The model utilizes MSC SINDA as a heat transfer solver with imbedded FORTRAN computer code to direct laser motion, apply laser heating as a boundary condition, and simulate the addition of metal powder layers during part fabrication. Model results are compared to available data collected during in situ DMLS part manufacture.
Document ID
20140016493
Acquisition Source
Marshall Space Flight Center
Document Type
Conference Paper
Authors
Cross, Matthew
(NASA Marshall Space Flight Center Huntsville, AL, United States)
Date Acquired
November 20, 2014
Publication Date
September 3, 2014
Subject Category
Metals And Metallic Materials
Report/Patent Number
M14-3734
Meeting Information
Meeting: JANNAF Additive Manufacturing for Propulsion Applications Technical Interchange Meeting (TIM)
Location: Huntsville, AL
Country: United States
Start Date: September 3, 2014
End Date: September 5, 2014
Sponsors: Department of the Air Force, Department of the Army, NASA Headquarters, Department of the Navy
Distribution Limits
Public
Copyright
Work of the US Gov. Public Use Permitted.
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