Ultralight and Very Light Helicopter Rotor Data
By:
References
- [1] rand, O. and khromov, V. Helicopter Sizing by Statistics. American Helicopter Society, 58th Annual Forum. Montreal, Canada (2002).
- [2] raymer, D. Aircraft Design: A Conceptual Approach, 3rd ed. American Institute of Aeronautics and Astronautics, Inc., reston, Virginia (1999).
- [3] Fradenburg, e. “the First 50 years Were Fine But What Should we do for an encore? Alexander A. Nicolsky Lecture.” Journal of American Helicopter Society (1994). p.3–20.
- [4] krenik, A. and Weiand, P. Aspects on Conceptual and Preliminary Helicopter Design. Deutscher Luft- und raumfahrtkongress, Document 420207 (2016).
- [5] Losev, L. Preliminary Determination of the Helicopter General Parameters Under Criteria of take-off Mass Minimum. kharkov Aviation Institute, kharkov (1988).
- [6] Losev, L. and ryabkov, V. Choice of The Coaxial Helicopter Parameters Under Criteria of Take-off Mass Minimum, kharkov Aviation Institute, kharkov (1999).
- [7] tishchenko, M. Choice of The Helicopter Parameters At The Preliminary Stage of Design. Moscow Aviation Institute, Moscow (2010).
- [8] Johnson, W. Design and Analysis of Rotorcraft. NASA/TP—2015–218751, NACA, Ames research Center, (2015).
- [9] Xin-Lai, L., Hu, L., Gang-Lin, W., and Zhe, W. “Helicopter Sizing Based on Genetic Algorithm Optimized Neural Network, Chinese.” Journal of Aeronautics Vol. 19 No. 3 (2006). p. 212–218.
DOI: https://doi.org/10.2478/tar-2023-0008 | Journal eISSN: 2545-2835
Language: English
Page range: 17 - 24
Submitted on: Oct 28, 2022
Accepted on: Mar 2, 2023
Published on: Jun 12, 2023
Published by: Sciendo
In partnership with: Paradigm Publishing Services
Publication frequency: 4 issues per year
Keywords:
Related subjects:
© 2023 Vitaly Dudnik, Victor Karabut, published by Sciendo
This work is licensed under the Creative Commons Attribution-NonCommercial-NoDerivatives 4.0 License.