This work is licensed under the Creative Commons Attribution-NonCommercial-NoDerivatives 4.0 International License.
[1] rand, O. and khromov, V. Helicopter Sizing by Statistics. American Helicopter Society, 58th Annual Forum. Montreal, Canada (2002).randO. and khromovV.Helicopter Sizing by Statistics.American Helicopter Society, 58th Annual Forum.Montreal,Canada(2002).Search in Google Scholar
[2] raymer, D. Aircraft Design: A Conceptual Approach, 3rd ed. American Institute of Aeronautics and Astronautics, Inc., reston, Virginia (1999).raymerD.Aircraft Design: A Conceptual Approach,3rd ed.American Institute of Aeronautics and Astronautics, Inc.,reston, Virginia(1999).Search in Google Scholar
[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.Fradenburge. “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.Search in Google Scholar
[4] krenik, A. and Weiand, P. Aspects on Conceptual and Preliminary Helicopter Design. Deutscher Luft- und raumfahrtkongress, Document 420207 (2016).krenikA and WeiandP.Aspects on Conceptual and Preliminary Helicopter Design.Deutscher Luft- und raumfahrtkongress, Document 420207 (2016).Search in Google Scholar
[5] Losev, L. Preliminary Determination of the Helicopter General Parameters Under Criteria of take-off Mass Minimum. kharkov Aviation Institute, kharkov (1988).LosevL.Preliminary Determination of the Helicopter General Parameters Under Criteria of take-off Mass Minimum.kharkov Aviation Institute,kharkov(1988).Search in Google Scholar
[6] Losev, L. and ryabkov, V. Choice of The Coaxial Helicopter Parameters Under Criteria of Take-off Mass Minimum, kharkov Aviation Institute, kharkov (1999).LosevL and ryabkovV.Choice of The Coaxial Helicopter Parameters Under Criteria of Take-off Mass Minimum,kharkov Aviation Institute,kharkov(1999).Search in Google Scholar
[7] tishchenko, M. Choice of The Helicopter Parameters At The Preliminary Stage of Design. Moscow Aviation Institute, Moscow (2010).tishchenkoM.Choice of The Helicopter Parameters At The Preliminary Stage of Design.Moscow Aviation Institute,Moscow(2010).Search in Google Scholar
[8] Johnson, W. Design and Analysis of Rotorcraft. NASA/TP—2015–218751, NACA, Ames research Center, (2015).JohnsonW.Design and Analysis of Rotorcraft. NASA/tP—2015-218751,NACA, Ames research Center, (2015).Search in Google Scholar
[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.Xin-LaiLHuLGang-LinW., and ZheW. “Helicopter Sizing Based on Genetic Algorithm Optimized Neural Network, Chinese.”Journal of AeronauticsVol.19No.3(2006). p.212-218.Search in Google Scholar