Aerodynamic Design for an Isolated Three-Dimensional Wing of an Unmanned Aerial Vehicle

STEPANOV, Kirill Aleksandrovich

doi:10.17223/19988621/54/10

Tomsk State University Journal of Mathematics and Mechanics

2016

DOI: 10.17223/19988621/54/10

|View full text |Cite

Aerodynamic Design for an Isolated Three-Dimensional Wing of an Unmanned Aerial Vehicle

Kirill Aleksandrovich STEPANOV¹

Abstract: Для аэродинамического проектирования трехмерного крыла беспилотного летательного аппарата среднего класса используется новая технология оптимального проектирования аэродинамических конфигураций на основе программного продукта нового поколения. Оптимальная форма крыла, обладающая минимальным полным сопротивлением при фиксированном коэффициенте подъемной силы и отвечающая заданным геометрическим и аэродинамическим ограничениям, определяется на основе глобального метода поиска и численных решений полных уравнений… Show more

Help me understand this report

Search citation statements

Order By: Relevance

Paper Sections

Select...

Citation Types

Supporting

Mentioning

Contrasting

Year Published

2020

Publication Types

Select...

Article1

Relationship

Self Cite0

Independent1

Authors

Journals

Cited by 1 publication

References 2 publications

(3 reference statements)

Supporting

Mentioning

Contrasting

Order By: Relevance

The development of a cloud system for investigation of UAVs aerodynamic characteristics

Kagenov

Kostyushin

Ismailov

et al. 2020

J. Phys.: Conf. Ser.

View full text Add to dashboard Cite

The paper presents the results of the development of a cloud system for multi-parameter aerodynamic calculations of unmanned aerial vehicles (UAVs). The developed cloud system consists of the following functional parts: web client – provides an access to the computing cloud, allows interactively preparing a task, sending prepared data to a computing cluster, getting and visualizing calculation results; and computing cloud – provides communication with the web client using an open API and manages the computing process. The computing process of the cloud is based on using open technologies of the OpenFOAM software adapted for solving aerodynamics problems. The authors carried out parametric studies of the external flow of UAV at free-stream velocities of 20, 25, 30 m/s with angles of attack from –4 to 12 degrees. It was found that the smallest drag force is observed for 0-3 degrees of the angle of attack of the flying wing, and the best lift to drag ratio is detected for 5 degrees attack angle. For 5 degrees attack angle the lift force is 47 N for an air free-stream velocity 20 m/s, 74 N – 25 m/s, 106 N – 30 m/s.

show abstract

The development of a cloud system for investigation of UAVs aerodynamic characteristics

Kagenov

Kostyushin

Ismailov

et al. 2020

J. Phys.: Conf. Ser.

View full text Add to dashboard Cite

show abstract

scite is a Brooklyn-based organization that helps researchers better discover and understand research articles through Smart Citations–citations that display the context of the citation and describe whether the article provides supporting or contrasting evidence. scite is used by students and researchers from around the world and is funded in part by the National Science Foundation and the National Institute on Drug Abuse of the National Institutes of Health.

Contact Info

hi@scite.ai

10624 S. Eastern Ave., Ste. A-614

Henderson, NV 89052, USA

Blog Terms and Conditions API Terms Privacy Policy Contact Cookie Preferences Do Not Sell or Share My Personal Information

Made with 💙 for researchers

Part of the Research Solutions Family.

Aerodynamic Design for an Isolated Three-Dimensional Wing of an Unmanned Aerial Vehicle

Cited by 1 publication

References 2 publications

The development of a cloud system for investigation of UAVs aerodynamic characteristics

The development of a cloud system for investigation of UAVs aerodynamic characteristics

Contact Info

Product

Resources

About