Average Ratings 0 Ratings
Average Ratings 0 Ratings
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
No
API Access
Has API
No
Integrations
No details available.
Integrations
No details available.
Pricing Details
$495 per year
Free Trial
Yes
Free Version
No
Pricing Details
Free
Free Trial
No
Free Version
Yes
Deployment
Web-Based
No
On-Premises
No
iPhone App
No
iPad App
No
Android App
No
Windows
Yes
Mac
No
Linux
No
Chromebook
No
Deployment
Web-Based
No
On-Premises
No
iPhone App
No
iPad App
No
Android App
No
Windows
Yes
Mac
Yes
Linux
Yes
Chromebook
No
Customer Support
Business Hours
No
Live Rep (24/7)
No
Online Support
Yes
Customer Support
Business Hours
No
Live Rep (24/7)
No
Online Support
Yes
Types of Training
Training Docs
No
Webinars
Yes
Live Training (Online)
No
In Person
No
Types of Training
Training Docs
Yes
Webinars
No
Live Training (Online)
No
In Person
No
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
No
3D Modeling
No
Chemical Engineering
No
Civil Engineering
No
Collaboration
No
Design Analysis
No
Design Export
No
Document Management
No
Electrical Engineering
No
Mechanical Engineering
No
Mechatronics
No
Presentation Tools
No
Structural Engineering
No