Processed data for "Effect of wingbeat frequency and stroke plane angle on aerodynamic efficiency and stability in hovering flight"

The data were obtained from a validated computational framework integrating high-fidelity aerodynamic (CFD) simulation with linearized flight-dynamics analysis of hovering hawkmoth flight.

Kinematic conditions were generated by independently varying the wingbeat frequency and the stroke plane angle from the measured natural kinematics, while maintaining the force balance required for hovering (the trim condition). For each condition, the files provide the trimmed kinematics, the aerodynamic forces and mechanical power, the aerodynamic stability derivatives, and the eigenvalues of the linearized system, together with the reduced lateral-model sensitivities used in the Supplementary Material.