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Uncertainty Analysis of Coaxial Thermocouple Calorimeters Used in Arc JetsRecent introduction of Coaxial Thermocouple type calorimeters into the NASA Ames arc jet facilities has inspired an analysis of 2D conduction effects internal to this type of calorimeter. Lateral conduction effects violate the 1D finite slab inverse analysis which is typically used to deduce the heat transfer to such calorimeters. The spherical shaped nose associated with most calorimeters (rather than flat) leads to a bias error that over-estimates the stagnation heating. Non-uniform heating on the face of spherically shaped calorimeters leads to conduction losses to the colder rim of the calorimeter which causes an underestimate of the stagnation heating. These two effects come into play at different times of the calorimeter's exposure to the arc jet, so they do not cancel. The spherical body effects come into play in the early stages of exposure, while the non-uniform heating effect becomes most severe at the later stages of exposure. The bias associated with spherical effects can be avoided by rewriting the 1D finite slab inverse analysis code to solve for 1D conduction in spherical coordinates. However, reducing the bias error associated non-uniform heating requires a somewhat ad hoc modification to the 1D finite element inverse analysis.
Document ID
20180007695
Acquisition Source
Ames Research Center
Document Type
Conference Paper
Authors
David M Driver
(Ames Research Center Mountain View, United States)
Daniel Philippidis
(Jacobs (United States) Dallas, Texas, United States)
Imelda Terrazas-Salinas
(Ames Research Center Mountain View, United States)
Date Acquired
November 14, 2018
Publication Date
June 25, 2018
Publication Information
Publication: 2018 Joint Thermophysics and Heat Transfer Conference
Publisher: American Institute of Aeronautics and Astronautics
e-ISBN: 9781624105524
Subject Category
Fluid Mechanics And Thermodynamics
Report/Patent Number
AIAA-2018-3770
ARC-E-DAA-TN56234
Meeting Information
Meeting: AIAA Aviation Forum
Location: Atlanta, GA
Country: US
Start Date: June 25, 2018
End Date: June 29, 2018
Sponsors: American Institute of Aeronautics and Astronautics
Funding Number(s)
CONTRACT_GRANT: NNA16BD26C
Distribution Limits
Public
Copyright
Public Use Permitted.
Technical Review
NASA Technical Management
Keywords
Isotherms
Finite Element Analysis
Stagnation Point
Spherical Shell
ANSYS
Spherical Coordinates
NASA Ames Research Center
Heat Transfer Modeling
Inverse Heat Conduction
Thermocouples
Coaxial TC
Calorimeter
Uncertainty
Arc Jet
Lateral Conduction
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