Dynamics of a high-authority active flap rotor

Annual Forum Proceedings - AHS International

Volumn 2, Issue , 2012, Pages 1102-1115

  Wong, Jonathan ^a,b   Andrews, Joseph ^a   Brigley, Mikel ^a  

^a SIKORSKY AIRCRAFT CORPORATION   (United States)

^b Dynamics and Internal Acoustics ^*  (United States)

Author keywords

[No Author keywords available]

Indexed keywords

ACTIVE CONTROL; ACTIVE FLAPS; ACTIVE ROTOR; AERODYNAMIC PERFORMANCE; AEROELASTIC STABILITY; CLOSED-LOOP; FLUTTER INSTABILITY; FREQUENCY DOMAINS; GROUND RESONANCE; HUB LOADS; TEST AND ANALYSIS; TESTING CONDITIONS; TORSION MODE; TRAILING EDGES; VIBRATION SUPPRESSION; WIND TUNNEL TESTS; WIND-TUNNEL TESTING;

ACTUATORS; AERODYNAMICS; HELICOPTERS; STRUCTURAL DYNAMICS; WIND STRESS;

SOFTWARE TESTING;

EID: 84864919298     PISSN: 15522938     EISSN: None     Source Type: Conference Proceeding    
DOI: None     Document Type: Conference Paper

References (9)

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3. Whirl and Wind Tunnel Testing of the Sikorsky Active Flap Demonstration Rotor. Lorber, P, et al. Virginia Beach, VA : American Helicopter Society 67th Annual Forum, May 3-5, 2011.
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9. Real-Time Extraction of Rotor Model Information for Stability Monitoring and Correlation. Andrews, J and Wong, J. San Francisco, CA : American Helicopter Society Specialists Meeting, January, 2012.