Simulation model for tail rotor failure

Simulation model for tail rotor failure

A helicopter simulation model, DYN, has been formulated to analyze helicopter flight response to tail rotor failure and steady flight recovery. The model uses classical rotor theory and integrates the nonlinear Euler equations of motion.

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Bibliographische Detailangaben
Veröffentlicht in:Journal of aircraft 1994-01, Vol.31 (1), p.197-205
1. Verfasser: O Rourke, Matthew J
Format: Artikel
Sprache:eng
Schlagworte:
Aerodynamics
Exact sciences and technology
Fracture mechanics (crack, fatigue, damage...)
Fracture mechanics, fatigue and cracks
Fundamental areas of phenomenology (including applications)
Helicopters
Physics
Simulation
Solid mechanics
Structural and continuum mechanics
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Beschreibung
Zusammenfassung:A helicopter simulation model, DYN, has been formulated to analyze helicopter flight response to tail rotor failure and steady flight recovery. The model uses classical rotor theory and integrates the nonlinear Euler equations of motion.
ISSN:0021-8669
1533-3868
DOI:10.2514/3.46474