Aerodynamic Interference between Main Rotor and Side Propellers of a Winged-type Compound Helicopter in Hover

Author:

KIMURA Keita1,SUGAWARA Hideaki1,TANABE Yasutada1

Affiliation:

1. Japan Aerospace Exploration Agency (JAXA)

Publisher

Japan Society for Aeronautical and Space Sciences

Subject

Space and Planetary Science,Aerospace Engineering

Reference21 articles.

1. 1) Lockheed Martin: Lockheed Martin Future Vertical Lift, https://www.lockheedmartin.com/fvl/index.html (Accessed 21 March 2022)

2. 2) Walsh, D., Weiner, S., Bagai, A., Lawrence, T., and Blackwell, R.: Development Testing of the Sikorsky X2 Technology Demonstrator, American Helicopter Society 65th Annual Forum, Test & Evaluation II Paper #2, 2009.

3. 3) Airbus: Airbus Helicopters Reveals Racer High-speed Demonstrator, 20 June 2017, https://www.airbus.com/newsroom/press-releases/en/2017/06/Airbus-Helicopters-reveals-Racer-high-speed-demonstrator-configuration.html (Accessed 11 July 2021)

4. 4) KHI: Kawasaki Heavy Industry HP, https://www.khi.co.jp/pressrelease/detail/20201006_1.html (Accessed 6 May 2021)

5. 5) Tanabe, Y., Aoyama, T., Kobiki, N., Sugiura, M., Miyashita, R., Sunada, S., Kawachi, K., and Nagao, M.: A Conceptual Study of High Speed Rotorcraft, 40th European Rotorcraft Forum, Southampton, UK, September, 2014, Proceedings, pp. 1111–1117.

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