LOFTID Aeroshell Thermal Response Uncertainty Analysis utilizing the End-to-End Monte Carlo Approach
Author:
Affiliation:
1. NASA Langley Research Center
Publisher
American Institute of Aeronautics and Astronautics
Link
https://arc.aiaa.org/doi/pdf/10.2514/6.2024-1499
Reference21 articles.
1. Probabilistic Design Demonstration of a Flexible Thermal Protection System for a Hypersonic Inflatable Aerodynamic Decelerator
2. Dec, J. A. and Mitcheltree, R. A. "Probabilistic Design of a Mars Sample Return Entry Vehicle Thermal Protection System," AIAA Paper 2002-0910. https://doi.org/10.2514/6.2002-910.
3. Probabilistic Modeling of Aerothermal and Thermal Protection Material Response Uncertainties
4. Iman, R. L., and Shortencarier, M. J. "A Fortran 77 Program and User's Guide for the Generation of Latin Hypercube and Random Samples for Use with Computer Models," NUREG/CR-3624, Technical Report SAND83-2365, Sandia National Laboratories, Albuquerque, NM, 1984.
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