Top-down view of the rotor. Blue arrows are the free-stream wind; red vectors show lift and orange shows drag at each blade. Blade color tracks Cp / Cp,peak (green → orange → red).
$$P = \tfrac{1}{2}\,\rho\,A\,V_\infty^{3}\,C_p,\qquad \mathrm{TSR}=\lambda=\frac{\omega R}{V_\infty},\qquad \sigma=\frac{N\,c}{2\pi R}$$
P: output power [W], ρ: air density (1.225 kg/m³), A: swept area (2RH for a VAWT), V_∞: free-stream wind speed [m/s], C_p: power coefficient (Betz limit 16/27 ≈ 0.593), λ: tip speed ratio, σ: solidity, N: blade count, c: blade chord, R: rotor radius.
$$C_p(\lambda)\approx C_{p,\mathrm{peak}}\left[1-\left(\frac{\lambda-\lambda_{\mathrm{opt}}}{\lambda_{\mathrm{opt}}}\right)^{2}\right]_{+}$$
Empirical Cp(λ) approximation: parabolic around the optimal TSR. Typical values are Darrieus H-rotor C_p,peak ≈ 0.43 at λ_opt ≈ 4, and Savonius C_p,peak ≈ 0.18 at λ_opt ≈ 0.8.