федеральное государственное автономное образовательное учреждение высшего образования
«Самарский национальный исследовательский университет имени академика С.П. Королева»

Grigorev, Vladimir A.

  • leading researcher
  • Department of Aircraft Engine Theory, professor
2019
  • 1 Kalabukhov D. S. , Grigoriev V.A., Zagrebelnyi A.O. etc. Updating the helicopter gas turbine engine mass model for the defining of the turboshaft engine optimal operating cycle parameters // Proceedings of the ASME Turbo Expo. — 2019. — Vol. 1.
  • 2 Grigor’ev V.A., Zagrebel’nyi A.O. Stability of Decisions in Choosing the Operating Parameter Values of the Gas Turbine Engine in the Helicopter System at the Initial Design Stage // Russian Aeronautics 2019. — Vol. 62. Issue 1. — P. 163-166
2018
  • 1 Kalabukhov D. S. , Radko V.M., Grigoriev V.A. Optimizing Parameters of Axial Pressure-Compounded Ultra-Low Power Impulse Turbines at Preliminary Design // IOP Conference Series: Materials Science and Engineering. — 2018. — Vol. 302. Issue 1.
2017
  • 1 Kalabukhov D. S. , Grigoriev V.A., Rad'ko V.M. Selecting rational parameters for ultra-low power two-stage axial turbine with pressure stages // Proceedings of the ASME Turbo Expo. — 2017. — Vol. 2C-2017.
  • 2 Grigor’ev V.A., Zagrebelnyy A.O. Influence of the helicopter flight design speed on the selection of working process parameters for GTE // Russian Aeronautics 2017. — Vol. 60. Issue 2. — P. 214-218
2015
  • 1 Grigoriev V.A., Rad'ko V.M., Kalabukhov D.S. Представление характеристик малоразмерных турбин энергетических установок // Aviatsionno-kosmicheskaya tekhnika i tekhnologiya 2015. — № № 7(124). — P. 77-83
  • 2 Grigor’ev V.A., Kalabukhov D. S. , Rad’ko V.M. Application of neural network approximation methods in the generalization and presentation of the aircraft gas turbine engine turbomachinery characteristics // Russian Aeronautics 2015. — Vol. 58. Issue 1. — P. 48-53
2014
  • 1 Grigor’ev V.A., Zagrebelnyy A.O. The problem of determining the design parameters of the gas turbine engine for a helicopter // Russian Aeronautics 2014. — Vol. 57. Issue 3. — P. 272-275
  • 2 GRECKOV A.I., Grigorev V.A, Zagrebelniy A.O. etc. К оценке аэродинамических характеристик вертолета в задаче выбора значений параметров рабочего процесса ГТД СТ // Aviatsionno-kosmicheskaya tekhnika i tekhnologiya 2014. — № 9 (116). — P. 17-20
1997
  • 1 Grigorev Vladimir Alekseevich, Dengov A.E. Optimization and Choice of parameters of working process small-size of the vehicle // China-Russia Sumposium on aeroengines. — 1997. — P. 65