THE AERODYNAMIC ANALYSIS OF THE PROFILES FOR FLYING WINGS
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 ar...
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Format: | Article |
Language: | English |
Published: |
Regional Department of Defense Resources Management Studies
2013-01-01
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Series: | Journal of Defense Resources Management |
Subjects: | |
Online Access: | http://journal.dresmara.ro/issues/volume4_issue1/24_prisacariu.pdf |
Summary: | 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. |
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ISSN: | 2068-9403 |