The Turbulence, Transition, and Numerical Method Technologies effort identifies and down-selects critical turbulence, transition, and numerical method capability improvements that enable at least a 40% reduction in predictive error against standard test cases. The project will examine turbulent separated flows, evolution of free shear flows, and shock-boundary layer interactions utilizing state-of-the-art high performance computing hardware.
More »The development of physics-based computational tools envisioned in Revolutionary Computational Aerosciences will yield a number of benefits: deliver a capability to the aeronautics community to improve designs and reduce design cycle times; accelerate introduction of advanced air vehicles and propulsion systems into the airspace system; enable simulation and certification by analysis, thereby reducing flight testing and resulting in savings of up to $1B from an aircraft development program.
More »Organizations Performing Work | Role | Type | Location |
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Glenn Research Center (GRC) | Lead Organization | NASA Center | Cleveland, Ohio |
Air Force Research Laboratory (AFRL) | Supporting Organization | Other US Government | Notre Dame, Indiana |
Massachusetts Institute of Technology (MIT) | Supporting Organization | Academia | Cambridge, Massachusetts |
Old Dominion University | Supporting Organization | Academia | Norfolk, Virginia |
Stanford University (Stanford) | Supporting Organization | Academia | Stanford, California |
The University of Texas at Austin | Supporting Organization | Academia | Austin, Texas |
University of Illinois at Urbana-Champaign | Supporting Organization | Academia | Urbana, Illinois |
University of Notre Dame (Notre Dame) | Supporting Organization | Academia | Notre Dame, Indiana |
University of Wyoming | Supporting Organization | Academia | Laramie, Wyoming |