SBIR/STTR Research Award

High-Resolution Unstructured Mesh Refinement Framework for Aircraft Icing Predictions

Award identifier 546959417f9a12c6f7a658e5b21f4c10269805982a9220ef3c3148c75cbcf29fAwarding agency National Aeronautics and Space Administration

Award amount

$149,962

Program and phase

SBIR · Phase I

Award year

2022

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Award details

Awarding agency
National Aeronautics and Space Administration
Branch
Not reported
Recipient company
CFD Research Corporation
Proposal award date
2022-07-21
Contract end date
2023-01-25
UEI
V3KCP1HNFM33
Solicitation number
SBIR_22_P1
Topic code
A1

Research abstract

Ice accretion on aircraft can trigger flow separation and degrade aerodynamic performance by reducing lift and stall angle-of-attack, increasing drag, and in severe cases causing complete loss of aircraft control. Modeling and quantification of icing effects on aircraft performance therefore plays a critical role in aircraft design and certification. High-fidelity CFD analyses of aircraft with imposed ice shapes are impeded by time-consuming manual pre-processing and mesh generation that are difficult to automate. Given the desire to adapt the mesh to optimize a given output functional (e.g. aircraft CLmax), these challenges are particularly important as the mesh quality in the vicinity of complex ice shapes directly impacts the accuracy of CFD solution error estimates. The objective of this project is to develop, demonstrate, and deliver a high-resolution automated unstructured mesh refinement framework for aircraft icing predictions. The capability will interface with existing NASA CFD solvers and provide access to high-resolution icing data in a manner consistent with established procedures for accessing CAD geometry, while locally disambiguating between CAD and ice shape. Grid quality improvements will be made near the complex ice geometry to improve error estimates. In Phase I, the capability will be developed in FUN3D using metric-based anisotropic mesh refinement to achieve optimal CLmax prediction for an iced aircraft configuration. Mesh refinement at the ice surface will be augmented to leverage the new API to query the true ice shape to improve the resolution of the surface discretization. Accuracy and efficiency of the developed capability will be demonstrated for a canonical wing geometry as proof of concept. Phase II efforts will further develop and mature the capability, and demonstrate on more complex topologies including high lift geometries and perform uncertainty quantification to understand and improve solution sensitivity and accuracy.

Technology keywords

Not reported

Other awards by this recipient

Verified by the same UEI. These are other public SBIR/STTR award pages, not a merged company record.

Research funding history

947 SBIR/STTR records share this UEI (1987–2026). Reported award amounts total $350,893,199. Reported amounts are not federal obligations.

Phases: Phase I, Phase II, Phase II – Direct to Phase II

Agencies: Department of Defense, National Aeronautics and Space Administration, Department of Health and Human Services, National Science Foundation, Department of Commerce, Department of Energy

Agency intelligence

National Aeronautics and Space Administration

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