| name | aerospace-engineering |
| description | Aerospace engineering fundamentals and applications |
| license | MIT |
| compatibility | opencode |
| metadata | {"audience":"engineers, developers, students","category":"engineering"} |
What I do
- Analyze aerodynamic forces and fluid dynamics around airframes and components
- Design and simulate aircraft structures, materials, and propulsion systems
- Calculate flight mechanics, stability, and control characteristics
- Evaluate propulsion systems including jet engines, turbines, and rockets
- Perform structural analysis using finite element methods
- Model orbital mechanics and spacecraft trajectories
When to use me
- When working on aircraft or spacecraft design projects
- When analyzing aerodynamic performance or fluid flow
- When calculating flight dynamics and control systems
- When evaluating structural integrity of aerospace components
- When designing propulsion systems or analyzing engine performance
- When modeling orbital trajectories or satellite operations
Key Concepts
Aerodynamics
Aerodynamics studies how air flows around objects and the forces generated:
L = 0.5 * rho * V**2 * S * Cl
D = 0.5 * rho * V**2 * S * Cd
Re = (rho * V * L) / mu
Where ρ = air density, V = velocity, S = wing area, Cl/Cd = coefficients.
Flight Mechanics
TR = W * (Cd0 + (K * Cl**2)) / Cl
n = 1 / cos(bank_angle)
R = (V / SFC) * (L/D) * ln(W_start / W_end)
Structural Analysis
sigma = E * epsilon
sigma_vm = sqrt(0.5 * ((s1-s2)**2 + (s2-s3)**2 + (s3-s1)**2))
FoS = Ultimate_Stress / Working_Stress
Orbital Mechanics
v = sqrt(mu / r)
v_esc = sqrt(2 * mu / r)
T = 2 * pi * sqrt(a**3 / mu)
Common Software Tools
| Tool | Purpose |
|---|
| ANSYS Fluent | CFD analysis |
| STAR-CCM+ | Multi-physics simulation |
| NASA OpenVSP | Vehicle preliminary design |
| AVL | aerodynamic prediction |
| JSBSim | flight dynamics simulation |