Abstract
A method for calculating available overloads and for subsequent evaluation of helicopter maneuverability is proposed taking into account specific operational conditions.
This is a preview of subscription content, log in via an institution to check access.
Similar content being viewed by others
References
Akimov, A.I., Berestov, L.M., and Mikheev R.A., Letnye ispytaniya vertoletov (Flight Tests of Helicopters), Moscow: Mashinostroenie, 1980.
Kalachev, G.S., Pokazateli manevrennosti, upravlyaemosti i ustoichivosti samoletov (Indicators of Aircraft Maneuverability, Controllability and Stability), Moscow: Oborongiz, 1958.
Mikhailov, S.A. and Onushkin, A.Yu., Power Balance Method in Calculation of Helicopter Maneuverability Taking into Account Specific Operational Conditions, Izv. Vuz. Av. Tekhnika, 2007, vol. 50, no. 2, pp. 7–11 [Russian Aeronautics (Engl.Transl.), 2007, vol. 50, no. 2, pp. 121–128].
Author information
Authors and Affiliations
Additional information
Original Russian Text © S.A. Mikhailov, Yu.P. Onushkin, A.A. Safonov, S.I. Kochish, 2009, published in Izvestiya VUZ. Aviatsionnaya Tekhnika, 2009, No. 2, pp. 32–35.
About this article
Cite this article
Mikhailov, S.A., Onushkin, Y.P., Safonov, A.A. et al. Numerical simulation of helicopter maneuverability in aerobatics research. Russ. Aeronaut. 52, 176–183 (2009). https://doi.org/10.3103/S1068799809020081
Received:
Published:
Issue Date:
DOI: https://doi.org/10.3103/S1068799809020081