Кафедра авіа- та ракетобудування

Lukianov Petro Volodymyrovych,

Associate Professor, Senior Researcher, Candidate of Physical and Mathematical Sciences

Teaching:

• Theory of Machines and Mechanisms.

• Machine Parts and Fundamentals of Design.

• Aerodynamics of Aircraft.

• Dynamics of Mechanical Structures of Airplanes, Helicopters, Satellites.

• Scientific work on the topic of the Master's thesis.

Education: Graduated from Taras Shevchenko National University of Kyiv, 1992, Department of Theoretical and Applied Mechanics. Major: Mechanics. Qualification: Mechanic.

In 1996, he defended his PhD thesis, and in 2014, he received the academic title of Senior Researcher. Main works related to aviation acoustics: study of the sound generation process of the interaction of helicopter blades and non-stationary inhomogeneous flow.

P.V. Lukianov is the author of a theoretical model of aerodynamic sound generation (2007), which is based on the Kelvin-Helmholtz theorem. Based on this model, a closed system of equations for the generation of aerodynamic sound in the general case was obtained. This system takes into account thermodynamic changes in the flow, therefore it can be used not only to describe the generation of sound by propeller aircraft, but also for the generation of sound by jet engines. For the numerical solution of problems of aviation acoustics, P.V. Lukyanov proposed a numerical-analytical method.

Main publications:

   Textbooks:

Lukianov P.V. Theory of machines and mechanisms. Practical classes. // Manual. - Electronic online educational publication. - KPI-2022, 104 p.).

Lukianov P. V. Aerodynamics of aircraft. Manual. - Electronic online educational publication. - KPI-2024, 188 p.

    Papers:

1. Lukianov P.V. A numerical method for Karman-Guderley equation. // VII International scientific conference “ AVIA-2006”, 25-27 September 2006,p.14.45-14.48.
2. Lukianov P.V. Unsteady propagation of small disturbances from a thin wing: The near and a far fields. // Acoustic bulletin. V.12,N3,2009,p.41-55.
3. Lukianov Petro V. Sound generation by Helicopter Blade Swept by Subsonic Flux. //Research Bulletin of the National Technical University of Ukraine “Kyiv Polytechnic Institue”. Ser.:phys. & math. Sciences N4(78),2011,p.143-148.
4. Lukianov P.V. On one numerically-analytical approach to solving of a problem on sound generation by a thin wing. Part I. General schematic of application to planer stationary problem. //Acoustic bulletin. V.14,N3,2011,p.46-52.
5. Lukianov Petr V. Sound generation by helicopter’s blade at oblique angle of flow blow. // Bulletin of Kyiv National University named after T.G.Shevchenko, Ser.:phys. & math. Sciences, N4,2011,p.91-94.
6. Lukianov P.V. Blade Shape and Cross Section’s Curvature Influence Parameters of the Rotor’s Rotational Noise// Research Bulletin of the National Technical University of Ukraine “Kyiv Polytechnic Institue”,N4(84),2012,p.149-153.
7. Lukianov P.V. On one numerically-analytical approach to solving of a problem on sound generation by a thin wing. Part II A schematic of application to non-stationary problems. //Acoustic bulletin. V.15,N3,2012,p.45-52.
8. Lukianov P.V. Sound of helicopter’s blade - vortex interaction. // Research Bulletin of the National Technical University of Ukraine “Kyiv Polytechnic Institue”. Ser.:phys. & math. Sciences,N4(90),2013,p.132-136.
9. Lukianov P.V. On one model for aeroacousics of viscous compressible gas.Part I Analysis of existing models,dedusing of resolving system of equations. //Acoustic bulletin. V.16,N2,2013-2014,p.18-30.
10. Lukianov P.V. On one model for aeroacousics of viscous compressible gas.Part II Noise of near helicopter blade-vortex interaction noise.// Acoustic bulletin. V.16,N3,2013-2014,p.31-40.
11. Lukianov P.V. Sound generation by Taylor and Scully Vortexes and the Blade of the Varing Cross Section. // Research Bulletin of the National Technical University of Ukraine “Kyiv Polytechnic Institue”. Ser.:phys. & math. Sciences,N4(96),2014,p.139-145.
12. Lukianov Petr V. Sound generation by blade and vortex near interaction at oblique angle of flow streamlining. // Bulletin of Kyiv National University named after T.G.Shevchenko, Ser.:phys. & math. Sciences, N4,2014,p.81-86.
13. Petro V. Lukianov. Helicopter’s rotor blade warp influence on BVI-noise generation. // Bulletin of Chercassy University, Ser.: applied mathematics & informatics, N38(331),2014,p.90-101.
14. P.V. Lukianov. Modeling the BVI-noise of two-blade helicopter rotor.//Acoustic bulletin. V.17,N1,2015,p.48-60.
15. P.V. Lukianov. Influence of blade tip rounding on level of BVI-noise.//Acoustic bulletin. V.17(2),2015,p.23-37.
16. P.V. Lukianov. Peculiarities of BVI-noise generation at helicopter’s airplane landing.// Bulletin of Zaporozhsky National University, ser.:phys. & math. Sciences, N2,2018,p.73-88.
17. Lukianov P.V. BVI-noise simulation of two-blade helicopter’s rotor sin-shape. // Visnyk of V.N. Karazin Kharkiv National University. Ser. “Mathematics, Applied Mathematics and Mechanics”.Vol.89,2019,p.59-75.
18. Lukianov P.V. BVI-noise generation by wing-shaped helicopter // Visnyk of V.N. Karazin Kharkiv National University. Ser. “Mathematics, Applied Mathematics and Mechanics”.Vol.91,2020,p.21-35.
19. Lukianov P.V. Pecularities of generation of BVI-noise of a helicopter rotor in “Vortex ring” mode. // Computer Science and Applied Mathematics-2021, N2,p.36-44.
20. Lukianov Petro, Dusheba Oleg. Modeling of aerodynamic noise of quadrotor type aerotaxi. // Aerospace technic and technology.-2023.-No.4 (188),p.38-49.
21. P.V.Lukianov, V.V.Kabanyachi. Mathematical Model of Stable Equilibrum operation of the flight simulator based on the Stewart platform.//Aviation.vol.27,No2(2023),p.119-128. (Scopus Q3) - https://journals.vilniustech.lt/index.php/Aviation/article/view/19264