Approach to modeling of thermal airflow dynamics

Suzdalev, Ivan; Stankūnas, Jonas; Komka, Arūnas

Use this URL to cite this publication: https://hdl.handle.net/20.500.14911/135065

Approach to modeling of thermal airflow dynamics

Details

Publication Type (CRIS)

Straipsnis Web of Science ir Scopus duomenų bazėje / Article in Web of Science and Scopus database (S1)

Publication Type (eLABa)

Straipsnis Web of Science DB / Web of Science DB article (S1)

Author(s)

Author	Affiliation
Suzdalev, Ivan	Aeronautikos inžinerijos katedra / Department of Aeronautical Engineering (0842)
Stankūnas, Jonas	Aeronautikos inžinerijos katedra / Department of Aeronautical Engineering (0842)
Komka, Arūnas	Metalinių ir kompozitinių konstrukcijų katedra / Department of Steel and Composite Structures (0259)

Title

Approach to modeling of thermal airflow dynamics

[en]

Ivan Suzdalev, Jonas Stankūnas, Arūnas Komka

Is part of

Journal of vibroengineering

Published In

Year	Volume	Issue	Start Page	End Page
2012	14	1	440	449

Publisher

Kaunas : Vibromechanika

Publisher (trusted)

Vibromechanika

Referenced in Database(s)(DBs)

Computers & Applied Sciences Complete (iki 2021 m.)

Science Citation Index Expanded (Web of Science)

VINITI RAN

SCOPUS

Extent

p. 440-449

URI

URI	Access Rights
https://hdl.handle.net/20.500.14911/135065
https://www.jvejournals.com/article/10595/pdf	Viso teksto dokumentas (atviroji prieiga) / Full Text Document (Open Access)

Cited references

Science / Art Area

Technologijos mokslai / Technological sciences (T)

Field of Science / Art

Transporto inžinerija / Transport engineering (T003)

Matavimų inžinerija / Measurement engineering (T010)

Keywords (en)

Abstract (en)

This work considers the modeling of thermal airflow. The dynamic airflow is spit on flat circular elements. The extrapolation method, which is referred to as adaptive extrapolation, is proposed. The extrapolation which is influenced by stochastically changing settings is the key for adaptive extrapolation. The change of these parameters is determined experimentally during real flight or using prediction techniques. This paper presents modeling with preset parameters. The thermal airflow is modeled by taking into account its inclination towards wind and the change of diameter in accordance with linear and nonlinear laws.