Aerodynamic characteristics of rigid coaxial rotor by wind tunnel test and numerical calculation

Author:

DENG Jinghui,FAN Feng,LIU Ping’an,HUANG Shuilin,LIN Yongfeng

Publisher

Elsevier BV

Subject

Mechanical Engineering,Aerospace Engineering

Reference21 articles.

1. Ruddell AJ. Advancing blade concept (ABC™) development. The 32nd annual national V/STOL forum of the American Helicopter Society. 1976.

2. Go JI, Park JS, Choi JS. Validation on conceptual design and performance analyses for compound rotorcrafts considering lift-offset. International Journal of Aeronautical & Space Sciences 2017; 18(1):154–64.

3. Harrington RD. Full-scale-tunnel investigation of the static-thrust performance of a coaxial helicopter rotor. Washington, D.C.: NASA; 1951. Report No.: NACA TN-2318.

4. Mosher M, Peterson RL. Acoustic measurements of a full-scale coaxial helicopter. AIAA 8th aeroacoustics conference. Reston: AIAA; 1983.

5. Fort F. An experimental investigation of hub drag on the XH-59A. Reston: AIAA; 1985. Report No.: AIAA-1985–4065.

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