F-0077-2021-16870: Wind Tunnel Test of Optimal Rotor Blade Tip for a Winged Compound Helicopter at High Advance Ratio - Technical Paper

Event: Vertical Flight Society 77th Annual Forum and Technology Display

Authors

Abstract

Content: ABSTRACT

Meta Tags

Topics: Wind tunnel tests
Helicopters
Propellers and rotors

Affiliated or Co-Author: Japan Aerospace Exploration Agency

Details

DOI: https://doi.org/10.4050/F-0077-2021-16870

Citation: Sugiura, M., Kimura, ., Kobiki, ., Sugawara, ., et al., "Wind Tunnel Test of Optimal Rotor Blade Tip for a Winged Compound Helicopter at High Advance Ratio," Vertical Flight Society 77th Annual Forum and Technology Display, Virtual, May 10, 2021, https://doi.org/10.4050/F-0077-2021-16870.

Additional Details

Publisher: The Vertical Flight Society

Published: 5/10/2021

Product Code: F-0077-2021-16870

Content Type: Technical Paper

Language: English