Analysis of the small flying wings performances in the morphing concept
Clicks: 116
ID: 41664
2017
Article Quality & Performance Metrics
Overall Quality
Not rated
Combines reader engagement with the AI quality analysis. This
article has not been analysed, so there is no overall score —
reader engagement is measured and shown alongside.
Reader Engagement
Steady Performance
30.0
/100
116 views
11 readers
AI Quality Assessment
Not analyzed
Readership in this journal
SteadyRanked #284 of 300 articles by views in matec web of conferences
Most read
Least read
Bar heights use a square-root scale. Only the 120 most-read articles are drawn; the journal has 300 in total.
Mint this article as an NFT
Not yet mintedCreate a permanent, verifiable on-chain record of this article on the Scimatic Network. The NFT is held in your Journament account, and you can withdraw it to your own wallet at any time.
5
SUSD
one-off · no wallet required
Abstract
Using of the flying wing (the UAVs category) in various fields (civilian and military) determine interests sustained of the aerodynamic and trajectory optimizations. The article presents analysis of wing flying performance (in morphing concept) by studying optimizing the maneuvers control and wind tunnel tests.
| Reference Key |
vasile2017analysismatec
Use this key to autocite in the manuscript while using
SciMatic Manuscript Manager or Thesis Manager
|
|---|---|
| Authors | Vasile, Prisacariu;Ionică, Cîrciu;Doru, Luculescu;Laurian, Gherman; |
| Journal | matec web of conferences |
| Year | 2017 |
| DOI |
DOI not found
|
| URL | |
| Keywords | Keywords not found |
Citations
No citations found. To add a citation, contact the admin at info@scimatic.org
Comments
No comments yet. Be the first to comment on this article.