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Average Ratings 0 Ratings

Total
ease
features
design
support

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Write a Review

Description

Conduct a swift and straightforward stability assessment of both surface and underground crown pillars, as well as laminated roof beds, through the utilization of three distinct limit equilibrium analysis techniques: rigid plate, elastic plate, and Voussoir (no tension) plate analysis. Additionally, carry out a probabilistic evaluation to ascertain the likelihood of failure by incorporating statistical distributions to account for variability in factors such as geometry, location of force application, joint and bedding strength, water pressure, external loads, and more. By executing a sensitivity analysis with a variety of values, you can assess how modifications to model parameters impact the factor of safety. The methodology, initially tailored for steeply dipping ore body configurations, allows for the estimation of crown geometry and the classification of stope geometry as either steep or shallow, thus enabling the application of the most relevant empirical relationships to your analysis. This comprehensive approach ensures a robust evaluation of stability across diverse geological conditions.

Description

NeuralWing serves as a cutting-edge model for real-time neural simulation and design optimization specifically tailored for transonic aircraft aerodynamics. It leverages the most comprehensive 3D transonic wing dataset, derived from 30,000 steady-state CFD simulations that span a 3D wing operating within the transonic regime, incorporating variations in four distinct geometry parameters and two different inflow conditions. By utilizing Emmi’s AB-UPT surrogate model, which has been meticulously trained on this extensive dataset, NeuralWing empowers users to effortlessly alter wing geometries, conduct optimizations, and enhance aerodynamic efficiency within mere seconds. The model is designed to facilitate transonic 3D wing simulations, accommodating variations in geometry and inflow, while offering real-time inference and optimization of design parameters. Users input a geometry mesh in STL format along with speed and angle of attack, and in return, they receive outputs that include pressure, friction, velocity fields, and integral forces such as lift and drag. Geometry meshes are generated dynamically in response to four design parameters, employing a differentiable approach that allows for swift assessment of design modifications. Furthermore, NeuralWing boasts an impressive accuracy rate of 99.5%, making it an invaluable tool for aerodynamics research and development. This level of precision ensures that engineers can trust the results as they iterate on their designs.

API Access

Has API

API Access

Has API

Screenshots View All

Screenshots View All

Integrations

No details available.

Integrations

No details available.

Pricing Details

$495 per year
Free Trial
Free Version

Pricing Details

Free
Free Trial
Free Version

Deployment

Web-Based
On-Premises
iPhone App
iPad App
Android App
Windows
Mac
Linux
Chromebook

Deployment

Web-Based
On-Premises
iPhone App
iPad App
Android App
Windows
Mac
Linux
Chromebook

Customer Support

Business Hours
Live Rep (24/7)
Online Support

Customer Support

Business Hours
Live Rep (24/7)
Online Support

Types of Training

Training Docs
Webinars
Live Training (Online)
In Person

Types of Training

Training Docs
Webinars
Live Training (Online)
In Person

Vendor Details

Company Name

Rocscience

Founded

1996

Country

Canada

Website

www.rocscience.com/software/cpillar

Vendor Details

Company Name

Emmi AI

Country

Austria

Website

www.emmi.ai/models/neuralwing

Product Features

Product Features

Engineering

2D Drawing
3D Modeling
Chemical Engineering
Civil Engineering
Collaboration
Design Analysis
Design Export
Document Management
Electrical Engineering
Mechanical Engineering
Mechatronics
Presentation Tools
Structural Engineering

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