Bepiločio orlaivio sparno profilių tyrimas

Lapušinskij, Aleksandr

Use this URL to cite this publication: https://hdl.handle.net/20.500.14911/140080

Bepiločio orlaivio sparno profilių tyrimas

Details

Publication Type (CRIS)

Straipsnis kitame recenzuojamame leidinyje / Article in other peer-reviewed edition (S5)

Publication Type (eLABa)

Straipsnis kitame recenzuotame leidinyje / Article in other peer-reviewed publication (S4)

Author(s)

Title

Bepiločio orlaivio sparno profilių tyrimas

[lt]

Aleksandr Lapušinskij

Title in other language

UAV wing airfoil aerodinamic analyses

[en]

Is part of

Aviacijos technologijos = Aviation technologies

Published In

Year	Volume	Issue	Start Page	End Page
2013	1	1	15	19

Publisher

Vilnius : Technika

Extent

p. 15-19

URI

URI	Access Rights
https://hdl.handle.net/20.500.14911/140080
Straipsnis	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)

Mechanikos inžinerija / Mechanical Engineering (T009)

Keywords (lt)

Keywords (en)

Abstract (lt)

Aptariamas Antano Gustaičio aviacijos institute gaminamo eksperimentinio bepiločio orlaivio sparno profilių tyrimas. Nagrinėjamos sparno profilio charakteristikos keičiant profilio santykinį gaubtumą. Parenkamas optimalus, tinkantis pasirinktam skrydžio greičių intervalui, sparno profilis.

Abstract (en)

The wing airfoils of an experimental UAV which is being designed at Antanas Gustaitis Aviation Institute is analysed and discussed. The wing airfoil characteristics when airfoil relative camber changes are being addressed. As a result, the most optimal wing airfoil used for targeted flight velocity interval is chosen.