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Apparent-Strain Correction for Combined Thermal and Mechanical TestingCombined thermal and mechanical testing requires that the total strain be corrected for the coefficient of thermal expansion mismatch between the strain gage and the specimen or apparent strain when the temperature varies while a mechanical load is being applied. Collecting data for an apparent strain test becomes problematic as the specimen size increases. If the test specimen cannot be placed in a variable temperature test chamber to generate apparent strain data with no mechanical loads, coupons can be used to generate the required data. The coupons, however, must have the same strain gage type, coefficient of thermal expansion, and constraints as the specimen to be useful. Obtaining apparent-strain data at temperatures lower than -320 F is challenging due to the difficulty to maintain steady-state and uniform temperatures on a given specimen. Equations to correct for apparent strain in a real-time fashion and data from apparent-strain tests for composite and metallic specimens over a temperature range from -450 F to +250 F are presented in this paper. Three approaches to extrapolate apparent-strain data from -320 F to -430 F are presented and compared to the measured apparent-strain data. The first two approaches use a subset of the apparent-strain curves between -320 F and 100 F to extrapolate to -430 F, while the third approach extrapolates the apparent-strain curve over the temperature range of -320 F to +250 F to -430 F. The first two approaches are superior to the third approach but the use of either of the first two approaches is contingent upon the degree of non-linearity of the apparent-strain curve.
Document ID
20070021456
Acquisition Source
Langley Research Center
Document Type
Conference Paper
Authors
Johnson, Theodore F.
(NASA Langley Research Center Hampton, VA, United States)
O'Neil, Teresa L.
(NASA Langley Research Center Hampton, VA, United States)
Date Acquired
August 23, 2013
Publication Date
April 23, 2007
Subject Category
Fluid Mechanics And Thermodynamics
Report/Patent Number
AIAA 2007-2410
Report Number: AIAA 2007-2410
Meeting Information
Meeting: 48th AIAA/ASME/ASCE/AHS/ASC Structures, Structural Dynamics, and Materials Conference
Location: Waikiki, HI
Country: United States
Start Date: April 23, 2007
End Date: April 26, 2007
Sponsors: American Helicopter Society, Inc., American Society of Mechanical Engineers, American Society of Civil Engineers, American Inst. of Aeronautics and Astronautics
Funding Number(s)
WBS: WBS 136905.08.05.04.05.04
Distribution Limits
Public
Copyright
Work of the US Gov. Public Use Permitted.
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