Effects of the shroud on aerodynamic performance in helicopter shrouded tail rotor system

Aircraft Engineering and Aerospace Technology

Volumn 73, Issue 6, 2001, Pages 568-572

  Xu, Guo Hua ^a   Wang, Shi Cim ^a  

^a NANJING UNIVERSITY OF AERONAUTICS AND ASTRONAUTICS   (China)

Author keywords

Aerodynamics; Helicopter services

Indexed keywords

AIRCRAFT PROPELLERS; AXIAL FLOW; DISKS (STRUCTURAL COMPONENTS); HELICOPTER ROTORS;

TAIL ROTOR SYSTEMS;

AERODYNAMICS;

EID: 0035780657     PISSN: 00022667     EISSN: None     Source Type: Journal    
DOI: 10.1108/00022660110408569     Document Type: Review

References (10)

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4. Meier, W.H., Groth, W.P. and Clark, D.R. (1975), "Flight testing of a fan-in-fin antitorque and directional control system and a collective force augmentation system", AD/A-013407.
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6. Mouille, R. (1986), "The 'fenestron' - a shrouded tail rotor concept for helicopters", presented at the 42nd Annual Forum of the American Helicopter Society, pp. 597-606.
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10. Wright, G., Driscoll, J.T. and Nickerson, J.D. Jr (1991), "Handling qualities of the H-76 fantail demonstrator", 47th Annual Forum of the American Helicopter Society, pp. 123-35.