Helicopter rotor icing protection systems are evaluated through flight tests under actual icing conditions. The development of a practical flight envelope which considers altitude, temperature, and icing severity is discussed. Flights without deicing protection are conducted to determine flight characteristics under total system failure.
Aerospatiale's Experience on Helicopter Flight in Icing Conditions
1983
10 pages
Report
Keine Angabe
Englisch
Helicopter flight characteristics in icing conditions
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