| dc.creator |
Vasile PRISACARIU |
|
| dc.date |
2013-01-01T00:00:00Z |
|
| dc.identifier |
2068-9403 |
|
| dc.identifier |
https://doaj.org/article/6a210a302eda48a590e6fc6fa8105fb9 |
|
| dc.description |
The possibility of using an un-piloted aerial vector is determined by the aerodynamic characteristics and performances. The design for a tailless unmanned aerial vehicles starts from defining the aerial vector mission and implies o series of geometrical and aerodynamic aspects for stability. This article proposes to remark the aerodynamic characteristics of three profiles used at flying wing airship through 2D software analysis. |
|
| dc.language |
EN |
|
| dc.publisher |
Regional Department of Defense Resources Management Studies |
|
| dc.relation |
http://journal.dresmara.ro/issues/volume4_issue1/24_prisacariu.pdf |
|
| dc.relation |
https://doaj.org/toc/2068-9403 |
|
| dc.source |
Journal of Defense Resources Management, Vol 4, Iss 1, Pp 211-218 (2013) |
|
| dc.subject |
Airfoil |
|
| dc.subject |
Flying Wing |
|
| dc.subject |
Aerodynamic Analysis |
|
| dc.subject |
Reynolds Number |
|
| dc.subject |
Military Science |
|
| dc.subject |
U |
|
| dc.subject |
DOAJ:Military Science |
|
| dc.subject |
DOAJ:Technology and Engineering |
|
| dc.title |
THE AERODYNAMIC ANALYSIS OF THE PROFILES FOR FLYING WINGS |
|
| dc.type |
article |
|
| dc.provenance |
Journal Licence: CC BY-NC-SA |
|