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Direct Reconstruction of Ablative Thermal Protection System Aeroheating Using A Green's Function Approach A Green’s function inverse heat transfer (IHT) approach is used to reconstruct the surface heating conditions on ablative thermal protection system (TPS) materials from embedded heat flux sensor and temperature probe measurements. The approach models the temperature time-history at the measurement location as a discrete linear system, allowing for the heat flux boundary condition to be recovered directly without the need for time-marching schemes. The effects of material decomposition and pyrolysis gas transport are modeled using an energy source/sink analogue. The performance of the reconstruction approach is analyzed on a 1D test case representative of an atmospheric entry heating scenario. The approach can recover the TPS surface heat flux to within 4% of the input heating condition with a computation time of 2-3 seconds (>3 orders of magnitude faster than current time-marching IHT methods). As a byproduct of the surface heating reconstruction, the algorithm also captures the surface pyrolysis gas mass flux and solid decomposition at multiple through-thickness locations within the TPS.
Document ID
20240013597
Acquisition Source
Ames Research Center
Document Type
Poster
Authors
Kenneth McAfee
(University of Maryland, College Park College Park, United States)
Hannah Alpert
(Ames Research Center Mountain View, United States)
Peter B Sunderland
(University of Maryland, College Park College Park, United States)
Oded Rabin
(University of Maryland, College Park College Park, United States)
Date Acquired
October 25, 2024
Subject Category
Aeronautics (General)
Meeting Information
Meeting: 14th Ablation Workshop 2024
Location: Laurel, MD
Country: US
Start Date: November 5, 2024
End Date: November 7, 2024
Sponsors: Johns Hopkins University Applied Physics Laboratory
Funding Number(s)
CONTRACT_GRANT: 80NSSC23K1201
WBS: 920121.01.02.01
Distribution Limits
Public
Copyright
Use by or on behalf of the US Gov. Permitted.
Technical Review
NASA Peer Committee
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