Influence of blade-to-blade dissimilarity on alleviation of helicopter blade-vortex interactions

Mathematical and Computer Modelling

Volumn 33, Issue 10-11, 2001, Pages 1139-1154

  Tauszig, L ^a   Gandhi, F ^a  

^a The Pennsylvania State University   (United States)

Author keywords

Blade vortex interactions; Dissimilar; Helicopter; Noise; Rotor

Indexed keywords

EID: 0035810137     PISSN: 08957177     EISSN: None     Source Type: Journal    
DOI: 10.1016/S0895-7177(00)00304-6     Document Type: Article

References (21)

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3. Some results of the testing of a full-scale Ogee-tip motor
4. Scissors rotor concept: New results obtained
5. Key results from a higher harmonic control aeroacoustic rotor test (HART)
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7. Reduction of helicopter BVI noise, vibration and power consumption through individual blade control
8. Flight tests of noise abatement approaches for rotorcraft using differential GPS guidance
9. Reduction of blade-vortex interaction (BVI) noise through X-force control
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11. A critical evaluation of various approaches for the numerical detection of helicopter blade-vortex interactions
12. Experimental and analytical predictions of rotor blade vortex interaction