Modeling Materials: Design for Planetary Entry, Electric Aircraft, and BeyondNASA missions push the limits of what is possible. The development of high-performance materials must keep pace with the agency's demanding, cutting-edge applications. Researchers at NASA's Ames Research Center are performing multiscale computational modeling to accelerate development times and further the design of next-generation aerospace materials. Multiscale modeling combines several computationally intensive techniques ranging from the atomic level to the macroscale, passing output from one level as input to the next level. These methods are applicable to a wide variety of materials systems. For example: (a) Ultra-high-temperature ceramics for hypersonic aircraft-we utilized the full range of multiscale modeling to characterize thermal protection materials for faster, safer air- and spacecraft, (b) Planetary entry heat shields for space vehicles-we computed thermal and mechanical properties of ablative composites by combining several methods, from atomistic simulations to macroscale computations, (c) Advanced batteries for electric aircraft-we performed large-scale molecular dynamics simulations of advanced electrolytes for ultra-high-energy capacity batteries to enable long-distance electric aircraft service; and (d) Shape-memory alloys for high-efficiency aircraft-we used high-fidelity electronic structure calculations to determine phase diagrams in shape-memory transformations. Advances in high-performance computing have been critical to the development of multiscale materials modeling. We used nearly one million processor hours on NASA's Pleiades supercomputer to characterize electrolytes with a fidelity that would be otherwise impossible. For this and other projects, Pleiades enables us to push the physics and accuracy of our calculations to new levels.
Document ID
20160003111
Acquisition Source
Ames Research Center
Document Type
Presentation
Authors
Thompson, Alexander (Universities Space Research Association Moffett Field, CA, United States)
Lawson, John W. (NASA Ames Research Center Moffett Field, CA United States)
Date Acquired
March 8, 2016
Publication Date
November 16, 2014
Subject Category
Aircraft Design, Testing And PerformanceNonmetallic Materials
Report/Patent Number
ARC-E-DAA-TN19084Report Number: ARC-E-DAA-TN19084
Meeting Information
Meeting: SC14: International Conference for High Performance Computing, Networking, Storage and Analysis