Measurement of Propeller Characteristics at a Negative Advance Ratio Using a Whirling Arm Facility

Author:

Itoh Yuto,Satoh Atsushi

Publisher

Springer Singapore

Reference10 articles.

1. Betzina M (2001) Tiltrotor descent aerodynamics: small-scale experimental investigation of vortex ring state. In: Proceedings of the 57th annual forum of the American Helicopter Society, 9–11 May 2001, Washington, DC, Fairfax, American Helicopter Society International

2. Gill AP, Battipede M (2001) Experimental validation of the wing dihedral effect using a whirling arm equipment. J Aircr. https://doi.org/10.2514/2.2874

3. Gina H (2013) Modeling ships and space craft: the science and art of mastering the oceans and sky. Springer, New York, pp 160–163

4. Keogh J, Barber T, Diasinos S, Doig G (2015) Techniques for aerodynamic analysis of cornering vehicles. SAE technical paper. https://doi.org/10.4271/2015-01-0022

5. Mulkens JMM, Ormerod OO (1993) Measurements of aerodynamics rotary stability derivatives using a whirling arm facility. J Aircr. https://doi.org/10.2514/3.48263

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