The Hong Kong Polytechnic UniversityDepartment of Aeronautical and Aviation EngineeringBack to the lab ↗

SOURCES & ATTRIBUTION

Rotor Unbalance & Critical Speed

Primary references and their specific role in this teaching laboratory. The diagrams and implementation are original.

Verification checks consistency with the declared equations. It does not establish experimental accuracy for an aircraft or facility.

Checked 23 October 2026 (UTC). Sources provide the physical concepts and educational context. The implementation, diagrams and parameter presets are original.

All default values and A/B presets are generic teaching assumptions. The source documents support the mechanisms; they do not experimentally validate this implementation. No manufacturer model, image, maintenance acceptance criterion or aircraft-specific vibration spectrum is distributed.