Helicopter Flight Simulation After Rotor Blade Failure for Accident Investigation
36th, Aerospace sciences meeting ; 1998 ; Reno; NV
01.01.1998
ALL
Nos AIAA 98-0001 to 98-1069 with gaps held only
Aufsatz (Konferenz)
Englisch
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Helicopter rotor behaviour after engine failure in foward flight
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|Failure of a Helicopter Main Rotor Blade
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|SIMULATION OF MAIN ROTOR BLADE LOADS IN HELICOPTER FLIGHT TRANSIENT CONDITIONS
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