Selected aerodynamic design issues for the single-rotor remotely piloted helicopter

Aircraft Engineering and Aerospace Technology

Volumn 72, Issue 3, 2000, Pages 241-246

  Guo, C G ^a   Xu, G H ^a  

^a NANJING UNIVERSITY OF AERONAUTICS AND ASTRONAUTICS   (China)

Author keywords

Aerodynamics; Design; Helicopters

Indexed keywords

EID: 0005104393     PISSN: 00022667     EISSN: None     Source Type: Journal    
DOI: 10.1108/00022660010332023     Document Type: Article

References (10)

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2. Faulkner, A.J. and Simons, I.A. (1977), "The remotely piloted helicopter", Vertica, Vol. 1 No. 3, pp. 231-8.
3. Fradenburgh, E.A. (1979), "Aerodynamic design of the Sikorsky S-76 SPIRIT helicopters", Journal of the American Helicopter Society, Vol. 24 No. 4, pp. 11-19.
4. Lynn, R.R. et al. (1970), "Tail rotor design part I: aerodynamics", Journal of the American Helicopter Society, Vol. 15 No. 4, pp. 2-15.
5. Mises, R.V. (1945), Theory of Flight, Chapter V, McGraw-Hill Book Company, Inc.
6. McCormick, B.W. (1967), Aerodynamics of V/STOL Flight, Chapter 2, Academic Press Inc.
7. Newman, S.J. (1994), The Foundations of Helicopter Flight, Edward Arnold.
8. Prouty, R.W. (1990), Helicopter Performance, Stability and Control, Robert E. Krieger Publishing Company.
9. Wiesner, W. and Kohler, G. (1973), "Tail rotor design guide", USAAMRDL TR 73-99.
10. Wright, G.P. and Lappos, N. (1981), "Sikorsky 76 helicopter handling qualities, design and development", Journal of the American Helicopter Society, Vol. 26 No.1, pp. 9-18.