The results of study and evaluation of a new design concept for helicopter tail rotors are reported. The evaluation was conducted by means of a whirl test which included separate runs at full pitch (19 DEG), overspeed to 110% rpm, and simulated forward flight to 105 knots. (Author)
Study and Evaluation of Directed Glass Fiber Reinforced Plastic Helicopter Tail Rotor Assembly
1969
66 pages
Report
Keine Angabe
Englisch
MM a. Tfiber-reinforced plastic helicopter tail rotor assembly (pultruded spar)
Tema Archiv | 1980
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