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Investigating and Analyzing Applied Loads Higher Than Limit LoadsThe results of the analysis for Balance 1621 indicate that the stresses are high near sharp corners. It is important to increase the size of the fillets to relieve some of the high stresses for the balances that will be designed. For the existing balances, the stresses are high and do not satisfy the established criteria. Two options are considered here. One is a possible modification of the existing balances, and two is to consider other load options. Redesigning a balance can be done in order to enhance the structural integrity of the balance. Because an existing balance needs to be modified, it is not possible to increase the fillet sizes without some further modifications to the balance. It is required that some materials be extracted from the balance in order to have larger fillet sizes. Researchers are interested in being able to apply some components of the load on the balance above the limit loads assigned. Is it possible to enhance the load on the same balance and maintain the factor of safety required? Some loads were increased above their limit loads and analyzed here.
Document ID
20040082241
Acquisition Source
Langley Research Center
Document Type
Preprint (Draft being sent to journal)
Authors
Karkehabadi, R.
(Lockheed Martin Corp. Hampton, VA, United States)
Rhew, R. D.
(NASA Langley Research Center Hampton, VA, United States)
Date Acquired
September 7, 2013
Publication Date
March 30, 2004
Subject Category
Structural Mechanics
Report/Patent Number
AIAA Paper 2004-2197
Report Number: AIAA Paper 2004-2197
Meeting Information
Meeting: 24th AIAA Aerodynamic Measurement Technology and Ground Testing Conference
Location: Portland, OR
Country: United States
Start Date: June 28, 2004
End Date: July 1, 2004
Sponsors: American Inst. of Aeronautics and Astronautics
Funding Number(s)
OTHER: 090-80-40
Distribution Limits
Public
Copyright
Work of the US Gov. Public Use Permitted.
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