Modeling and Numerical Investigation of Aerodynamic Characteristics of a Propeller Circling on a Whirling Arm
Author:
Affiliation:
1. Graduate School of Engineering, Iwate University
2. Faculty of Science and Engineering, Iwate University
Publisher
Japan Society for Aeronautical and Space Sciences
Subject
Space and Planetary Science,Aerospace Engineering
Link
https://www.jstage.jst.go.jp/article/tjsass/64/6/64_T-20-60/_pdf
Reference17 articles.
1. 1) Silvestre, M. A. R., Morgado, J., Alves, P., Santos, P., Gamboa, P., and Pascoa, J. C.: Propeller Performance Measurements at Low Reynolds Numbers, I. J. Mechanics, 10 (2015), pp. 154–166.
2. 2) Brandt, B. J. and Selig, S. M.: Propeller Performance Data at Low Reynolds Numbers, 49th AIAA Aerospace Sciences Meeting Including the New Horizons Forum and Aerospace Exposition, Orlando, Florida, United States of America, AIAA 2011-1255, 2011.
3. 3) Merchant, P. M. and Miller, S. L.: Propeller Performance Measurement for Low Reynolds Number UAV Applications, 44th AIAA Aerospace Sciences Meeting and Exhibit, Reno, Nevada, United States of America, AIAA 2006-1127, 2006.
4. 4) Itoh, Y.: Measurement of Propeller Characteristics at Low Advance Ratio Using a Whirling Arm with Brake, Proceedings of 55th Aircraft Symposium, Matsue, Japan, JSASS-2017-5023, 2017 (in Japanese).
5. 5) Itoh, Y. and Satoh, A.: Measurement of Propeller Characteristics at a Negative Advance Ratio Using a Whirling Arm Facility, The Proceedings of the 2018 Asia-Pacific International Symposium on Aerospace Technology (APISAT 2018), Lect. Notes Electr., 459 (2019), pp. 1169–1188.
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