• 560 Citations
  • 13 h-Index
1987 …2019
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Fingerprint Dive into the research topics where Sergey V Shkarayev is active. These topic labels come from the works of this person. Together they form a unique fingerprint.

  • 2 Similar Profiles
Micro air vehicle (MAV) Engineering & Materials Science
Aerodynamics Engineering & Materials Science
Angle of attack Engineering & Materials Science
Kinematics Engineering & Materials Science
Dissimilar materials Engineering & Materials Science
Wind tunnels Engineering & Materials Science
Vortex flow Engineering & Materials Science
Propellers Engineering & Materials Science

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Research Output 1987 2019

  • 560 Citations
  • 13 h-Index
  • 33 Article
  • 26 Conference contribution
  • 2 Chapter

Aerodynamic design of long-range vtol uav

Footohi, P., Bouskela, A. & Shkarayev, S. V., Jan 1 2019, AIAA Scitech 2019 Forum. American Institute of Aeronautics and Astronautics Inc, AIAA, (AIAA Scitech 2019 Forum).

Research output: Chapter in Book/Report/Conference proceedingConference contribution

Fuselages
Unmanned aerial vehicles (UAV)
Ground effect
Aerodynamics
Planforms

Aerodynamics of a wing with a wingtip flapper

Zhao, L., Shkarayev, S. V. & Su, E., Jun 1 2018, In : Fluids. 3, 2, 29.

Research output: Contribution to journalArticle

Open Access
aerodynamics
wings
Aerodynamics
Vortex flow
vortices
1 Citation (Scopus)

Flow studies around a small propeller in converting maneuver

Shkarayev, S. V., Kurnosov, V., Gomez, D., Jardin, T. & Moschetta, J. M., Jan 1 2017, 35th AIAA Applied Aerodynamics Conference, 2017. American Institute of Aeronautics and Astronautics Inc, AIAA, (35th AIAA Applied Aerodynamics Conference, 2017).

Research output: Chapter in Book/Report/Conference proceedingConference contribution

Propellers
Vortex flow
Angular momentum
Angle of attack
Unmanned aerial vehicles (UAV)

Modification of vortex identification method based on normalized angular momentum

Kurnosov, V. & Shkarayev, S. V., 2017, 33rd AIAA Aerodynamic Measurement Technology and Ground Testing Conference, 2017. American Institute of Aeronautics and Astronautics Inc, AIAA

Research output: Chapter in Book/Report/Conference proceedingConference contribution

Angular momentum
Vortex flow
Propellers
Invariance
Robustness (control systems)

Visualization of vortical flows around a rapidly pitching wing and propeller

Su, E., Randall, R., Wilson, L. & Shkarayev, S. V., Mar 1 2017, In : International Journal of Micro Air Vehicles. 9, 1, p. 25-43 19 p.

Research output: Contribution to journalArticle

Propellers
Vortex flow
Visualization
Angle of attack
Boundary layers