List of ANSYS FENSAP-ICE Customers
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Since 2010, our global team of researchers has been studying ANSYS FENSAP-ICE customers around the world, aggregating massive amounts of data points that form the basis of our forecast assumptions and perhaps the rise and fall of certain vendors and their products on a quarterly basis.
Each quarter our research team identifies companies that have purchased ANSYS FENSAP-ICE for 2D/3D Simulation from public (Press Releases, Customer References, Testimonials, Case Studies and Success Stories) and proprietary sources, including the customer size, industry, location, implementation status, partner involvement, LOB Key Stakeholders and related IT decision-makers contact details.
Companies using ANSYS FENSAP-ICE for 2D/3D Simulation include: Honeywell, a United States based Manufacturing organisation with 95000 employees and revenues of $36.66 billion, Bell Flight, a United States based Manufacturing organisation with 8000 employees and revenues of $1.50 billion, Safran Engineering Services, a France based Manufacturing organisation with 3700 employees and revenues of $500.0 million and many others.
Contact us if you need a completed and verified list of companies using ANSYS FENSAP-ICE, including the breakdown by industry (21 Verticals), Geography (Region, Country, State, City), Company Size (Revenue, Employees, Asset) and related IT Decision Makers, Key Stakeholders, business and technology executives responsible for the PLM and Engineering software purchases.
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| Logo | Customer | Industry | Empl. | Revenue | Country | Vendor | Application | Category | When | SI | Insight |
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Bell Flight | Manufacturing | 8000 | $1.5B | United States | Ansys Inc. | ANSYS FENSAP-ICE | 2D/3D Simulation | 2015 | n/a |
In 2015 Bell Flight implemented ANSYS FENSAP-ICE to support rotor ice shedding and trajectory analyses, aligning the deployment to its Fluid Product Engineering needs for rotorcraft aerodynamics and icing analysis. The ANSYS FENSAP-ICE implementation was positioned to address flow, droplet, ice accretion, shedding and post-shed trajectory evaluation as core engineering functions for hover and forward flight regimes.
The project established a Computational Fluid Dynamics framework that combined ANSYS FENSAP flow simulations with ANSYS DROP3D droplet field computation and ANSYS ICE3D ice accretion modeling. Rotor blades and shed-ice shapes were meshed in ANSYS ICEM, and a stitching methodology was used to perform rotor flow simulations in ANSYS FENSAP which separated stationary and rotating domains to capture rotorcraft-specific aerodynamic interactions.
Integration work included developer-authored Fortran code to determine shed location and time of shedding, and an aerodynamic database driven six degree of freedom model that used Reduced Order Modelling and elemental interpolation to investigate potential impact zones. The implementation linked meshing, flow, droplet, accretion and shedding outputs into the 6-DOF trajectory assessment to enable end-to-end ice shedding and impact analysis workflows.
Operational coverage focused on rotorcraft engineering teams performing analyses in both hover and forward flight, with processes orchestrated across meshing, CFD execution, droplet and ice modules, and trajectory post-processing. ANSYS FENSAP-ICE was restated in workflows to ensure the Fluid Product Engineering use case, and the deployment emphasized integrated module sequencing and model-based interpolation for impact zone assessments.
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Honeywell | Manufacturing | 95000 | $36.7B | United States | Ansys Inc. | ANSYS FENSAP-ICE | 2D/3D Simulation | 2012 | n/a |
In 2012, Honeywell implemented ANSYS FENSAP-ICE to simulate ice accretion for internal turbo-machinery, aligning the project with Fluid Product Engineering requirements for aero-thermal and icing analysis. The implementation centered on using ANSYS FENSAP-ICE as the primary code set to predict particle trajectory, impingement and mass caught in rotating and stationary turbomachinery components, supporting engineering decisions in turbomachinery design teams.
The technical configuration included the FensapIce3D module and Drop3D for ice accretion physics, combined with CFX particle capabilities within Ansys/CFX to provide coupled flow and particle transport solutions. A particle transport solution with a bouncing feature was implemented to increase fidelity of particle trajectory solutions, improving prediction of impingement locations and accumulated ice mass, and the solution workflow maintained explicit separation of flow field resolution, particle tracking, and ice growth modeling.
Integrations were focused on tight coupling between Ansys/CFX flow solvers and the FensapIce3D based icing modules, enabling exchange of flow field and particle impact data for iterative simulation runs. Operational scope targeted internal turbo-machinery engineering use cases, with workflows built for pre-processing mesh and drop field definition, runtime particle transport with bouncing physics, and post-processing of impingement maps and accretion geometry for downstream design evaluation.
Governance and process changes emphasized simulation-driven validation and repeatable analysis protocols, standardizing model setup, particle loading definition, and verification checks across turbomachinery projects. The ANSYS FENSAP-ICE implementation was positioned as an engineering simulation capability within Honeywell’s Fluid Product Engineering portfolio, supporting iterative design and aero-thermal assessment workflows rather than as a standalone testing practice.
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Safran Engineering Services | Manufacturing | 3700 | $500M | France | Ansys Inc. | ANSYS FENSAP-ICE | 2D/3D Simulation | 2014 | n/a |
In 2014 Safran Engineering Services implemented ANSYS FENSAP-ICE to advance icing modelling capabilities as part of an on-site CFD investigation at the Bordes facility supporting Safran Helicopter Engines. The deployment focused on Fluid Product Engineering use cases and was positioned alongside complementary CFD calibration work using ANSYS Fluent to validate aerodynamic behavior on helicopter engine air intakes.
The ANSYS FENSAP-ICE implementation concentrated on physics-aligned icing modelling workflows, including setup of ice accretion simulation cases, aerodynamic surface definition, and boundary condition configuration to support predictive icing studies. Configuration work emphasized reproducible CFD case management and mesh strategies consistent with engineering analysis practices in product and aerodynamic engineering.
Parallel activities included calibration of ANSYS Fluent for 3D aerodynamics calculations on a system composed of air intakes of two turbo engines installed on a helicopter, and evaluation of a Fluent module dedicated to modelling airflow through a helicopter rotor. These tasks involved direct numerical to experimental comparison, indicating an operational validation loop between numerical simulation outputs and test measurements conducted under the Safran Helicopter Engines assignment at Bordes.
Governance and rollout were executed as on-site engineering assignments, continuing an investigation that began during a final year placement, and therefore followed an iterative knowledge transfer and validation cadence between aircraft propulsion engineering teams and the CFD analysts. The program unified ANSYS FENSAP-ICE based icing analysis with Fluent aerodynamic calibration to support engineering decision making in Fluid Product Engineering workflows.
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Buyer Intent: Companies Evaluating ANSYS FENSAP-ICE
- Georgia Institute of Technology, a United States based Education organization with 14000 Employees
- Peregrine Avionics, a United States based Aerospace and Defense company with 70 Employees
Discover Software Buyers actively Evaluating Enterprise Applications
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