A comprehensive aerodynamics and fluid dynamics knowledge tool mapping everything from basic airfoil lift formulas to supersonic shock waves and CFD modeling.
The fastest way to install a skill directly from the registry.
npx clawhub@latest install ai-aerodynamics
Copy the skill folder to one of these locations
~/.openclaw/skills/ <project>/skills/ Priority: Workspace > Local > Bundled
Copy this prompt to OpenClaw to install it automatically.
Help me install ai-aerodynamics using Clawhub. If Clawhub is not installed, install it first (npm i -g clawhub).
Get the raw skill files in a ZIP archive.
The AI Aerodynamics Guide is a domain-specific core skill designed to help engineers, students, and automotive or aerospace enthusiasts understand, calculate, and analyze fluid dynamics problems. It covers essential foundations such as the Navier-Stokes equations, Reynolds number thresholds, and Mach speed behaviors, extending straight to practical aerodynamics applications like airfoil engineering and wind tunnel workflows.
By leveraging this guide within Openclaw Skills, users gain an interactive educational and research companion. It dissects complex concepts like boundary layer transitions, laminar flow airfoils, and the mathematics of lift generation without oversimplifying the underlying physics, unlocking actionable computational fluid dynamics insights.
To install and activate the fluid dynamics capabilities inside your Openclaw environment, execute the plugin management tool:
claw-cli install ai-aerodynamics
Verify that the environment variable configurations or local model routing profiles are updated to support physics-based reasoning prompts.
The skill manages information taxonomy across the following key aerodynamic domains:
| Domain Block | Core Concepts Managed | Metrics & Formulas Covered |
|---|---|---|
| Fluid Foundations | Navier-Stokes equations, Incompressible vs. Compressible flow | $Re = \frac{\rho VL}{\mu}$, $Ma = \frac{V}{a}$, Bernoulli Principle |
| Lift & Airfoils | Circulation, Angle of Attack, Stall, NACA Profiles | $L = \rho V \Gamma$, Kutta condition |
| Boundary Layers | Laminar vs. Turbulent layers, Transition, Separation | Adverse pressure gradient, Skin friction drag |
| Compressible Flow | Sound barrier, Shock waves, Mach angle, Area rule | $\mu = \arcsin(\frac{1}{Ma})$, Supercritical airfoils |
| CFD Engineering | Hexahedral/Tetrahedral Mesh, Model Validation (V&V) | DNS vs. LES vs. RANS models ($k-\epsilon$, $k-\omega$ SST) |
| Wind Tunnel Labs | Flow visualization (Schlieren, PIV, Oil flow), Force balances | 6-component balance, Similarity parameters |
| Industrial Design | Automotive Cd management, Sports ball drag, Wind turbines | Downforce, Dimple effects, Tip-speed ratio ($\lambda$) |
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