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Next-Gen Aerodynamic Cloud Computing

Optimizing Performance
Through Fluid Dynamics.

Lumina Dynamic brings high-fidelity CFD and airfoil analysis to your browser. Design faster, analyze deeper, and fly further with our integrated cloud workflow.

Trusted by Innovators

AI-Powered Solvers

Utilize NeuralFoil and XFOIL 6.99 for near-instant aerodynamic coefficient estimation.

STL-to-CFD Pipeline

Upload your 3D geometry and prepare mesh configurations for high-end cloud simulations.

Interactive Polars

Compare multiple airfoils side-by-side with real-time interactive charting and CSV exports.

End-to-End Design Pipeline

Comprehensive Aerodynamic Engineering.

Lumina Dynamic provides a seamless workflow from initial 2D profile selection to full 6-DOF flight dynamics testing. Stop switching between fragmented tools and scale your aerospace concepts in a unified, cloud-native environment.

Active

2D Airfoil Studio

Rapidly evaluate 1600+ Selig/NACA profiles or upload custom coordinate geometries (.DAT). Leverage thin-airfoil theory and empirical viscous corrections to generate high-fidelity lift, drag, and pitching moment polars instantly.

Cl/Cd/Cm Polars Viscous Flow
Active

3D Propeller Analytics

Upload your complex STL rotor geometries. Our solver slices the 3D mesh into radial stations and applies advanced Blade Element Momentum Theory (BEMT) to accurately calculate thrust, torque, and overall aerodynamic efficiency.

STL Parsing BEMT Solver
Coming Soon

Cloud CFD Pipeline

Automated, high-quality volume meshing directly from your uploaded CAD/STL files. Run massively parallelized Navier-Stokes simulations on our cloud clusters to visualize flow separation, pressure distribution, and wake turbulence.

Navier-Stokes Auto-Meshing
Coming Soon

6-DOF Flight Dynamics

Take the aerodynamic coefficients derived from the Airfoil and Propeller modules and plug them directly into our 6 Degrees of Freedom physics engine. Evaluate aircraft stability derivatives and control responses in real-time.

6-DOF Engine Stability Analysis
Compute Architecture

Powered by Industry-Standard Engines.

We bring heavy-duty aerospace computation directly to your browser. By combining classical aerodynamic solvers with modern machine learning and scalable cloud infrastructure, Lumina Dynamics eliminates the need for expensive local workstations.

NeuralFoil & XFOIL

Hybrid 2D solver architecture. We use NeuralFoil for near-instant AI-driven estimations, validated by the time-tested XFOIL 6.99 panel method for high-fidelity viscous and inviscid interactions.

BEMT + Wake Theory

Advanced rotorcraft analytics. Our propeller module utilizes Blade Element Momentum Theory (BEMT) coupled with advanced wake models to accurately predict inflow velocities and tip losses.

OpenFOAM

The backbone of our upcoming 3D CFD pipeline. We leverage OpenFOAM for robust, parallelized Navier-Stokes computations, combined with automated SnappyHexMesh generation for STL geometries.

Cloud & WebGL

A true cloud-native experience. High-performance computing powered by a FastAPI/Python distributed backend, with real-time hardware-accelerated 3D visualization using Three.js.

Cloud-Native

Zero Local Installation Required

Scalable

Distributed Parallel Computing

API-Ready

Integrate With Your Custom Pipeline

Early Access

Pricing Plans

Choose the right computational power for your engineering needs.

Payment Infrastructure Coming Soon

Detailed pricing tables, subscription plans, and payment integration will be added . For now, you can test it by clicking

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See how Lumina Dynamic can scale your aerodynamic workflow.

LUMINA DYNAMIC

PROTOTYPE V2.0

Welcome, ENGINEER

Select the module you want to test.

Airfoil Studio 2D

Airfoil analysis with neural foil theory.

Theory

Propeller Studio 3D

STL-to-propeller performance analysis.

BEMT + WAKE THEORY

CFD Analyser 3D

Coming Soon — Cloud CFD Analysis Pipeline.

Flight Simulator

In progress — Physics engine development.

Backend sunucusu bulunamadı — JS yaklaşım modeli kullanılıyor. Gerçek sonuçlar için uvicorn main:app --reload komutunu çalıştırın.

Stall Region
Thin Airfoil Theory + Stall Model

Add a profile and run analysis

Select or upload airfoil geometries from the sidebar to execute the solver.

Thrust (T)

0 N

Torque (Q)

0 Nm

Power (P)

0 kW

Solver Live Logs

Coming soon ...

3D INTERACTIVE RENDER

Model: Default Geometry

Drag to rotate