Technical note performance of a Sikorsky S-61 with a new main rotor

Journal of the American Helicopter Society

Volumn 48, Issue 3, 2003, Pages 211-215

  Curtiss Jr , H C ^a   Carson, Frank ^b   Hill, Jeff ^b   Quackenbush, Todd ^c  

^a PRINCETON UNIVERSITY   (United States)

^b Carson Helicopters   (United States)

^c Continuum Dynamics Inc ^*  (United States)

Author keywords

[No Author keywords available]

Indexed keywords

FLIGHT DYNAMICS; STRUCTURAL LOADS; TURBOMACHINE BLADES; VIBRATIONS (MECHANICAL);

CONTROL CHARACTERISTICS;

HELICOPTER ROTORS;

EID: 0042766994     PISSN: 00028711     EISSN: None     Source Type: Journal    
DOI: 10.4050/jahs.48.211     Document Type: Article

References (8)

1. Felker, F. F., Quackenbush, T. R., and Bliss, D. B., "Comparison of Predicted and Measured Rotor Performance in Hovering using a New Free Wake Analysis," Vertica, Vol. 14, (3), 1990.
2. Shanley, J. P., Moffitt, R. C., and Davis, S. J., "Systematic Correlation and Evaluation of the EHPIC Hover Analysis," American Helicopter Society 46th Annual Forum Proceedings, Washington, D.C., June 1990.
3. Gupta, B. P., "Blade Design Parameters which Affect Helicopter Vibrations," Paper No. A-84-40-23-6000, American Helicopter Society 40th Annual Forum Proceedings, Arlington, VA, May 1984.
4. Vincent, A. H., "Design and Development of the Sea King Composite Main Rotor Blade," Paper No. 6.1, 8th European Rotorcraft Forum Proceedings, Aix-En-Provence, France, September 1982.
5. Noonan, K. W., "Aerodynamic Characteristics of Two Rotorcraft Airfoils Designed for Application to the Inboard Region of a Main Rotor Blade," NASA TP 3009, July 1990.
6. Bingham, G. J., and Noonan, K. W., "Two-Dimensional Aerodynamic Characteristics of Three Rotorcraft Airfoils at Mach Numbers from 0.35 to 0.90," NASA TP 2000, 1982.
7. Beno, E. A., "Analysis of Helicopter Maneuver Loads and Rotor-Loads Flight-Test Data," NASA CR-2225, March 1973.
8. Anon., CH-3E/HH-3E Flight Manual, USAF.