Implementation of the problem described in:
Tribes, Dubé, Trépanier, Decomposition of multidisciplinary optimization
problems: formulations and application to a simplified wing design.
Engineering Optimization, 37(8):775–796, 2005.
- Input dimension: 7
- Number of constraints: 3
- Constraints must satisfy the form: gᵢ(x) ≤ 0
| x₁ | x₂ | x₃ | x₄ | x₅ | x₆ | x₇ | |
|---|---|---|---|---|---|---|---|
| Quantity | b | Cᵣ | λ | αᵣ | α₀ₜ | dᵣ | tᵣ |
| Lower bound | 30 | 6 | 0.28 | −1 | −1 | 1.6 | 0.30 |
| Upper bound | 45 | 12 | 0.50 | 3 | 3 | 5.0 | 0.79 |