Performance of a Mach-Scale Coaxial Counter-Rotating Rotor in Hover

Author:

Cameron Christopher G.1,Karpatne Anand1,Sirohi Jayant1

Affiliation:

1. University of Texas at Austin, Austin, Texas 78712

Publisher

American Institute of Aeronautics and Astronautics (AIAA)

Subject

Aerospace Engineering

Reference21 articles.

1. ColemanC. P. “A Survey of Theoretical and Experimental Coaxial Rotor Aerodynamic Research,” NASA TP-3675, 1997.

2. The ABC Helicopter

3. PhelpsA. E.MineckR. E. “Aerodynamic Characteristics of a Counter-Rotating, Coaxial, Hingeless Rotor Helicopter Model with Auxiliary Propulsion,” NASA TM-78705, May 1978.

4. ArentsD. N. “An Assessment of the Hover Performance of the XH-59A Advancing Blade Concept Demonstration Helicopter,” U.S. Army Air Mobility Research and Development Lab., TR USAAMRDL-TN-25, Fort Eustis, VA, May 1977.

5. FelkerF. F. “Performance and Loads Data from a Wind Tunnel Test of a Full-Scale, Coaxial, Hingeless Rotor Helicopter,” NASA TM-81329, Oct. 1981.

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