Application of boundary estimation method for determining aircraft aerodynamic parameters
<span lang="EN-US">Described is boundary estimation method of aircraft aerodynamic parameters which allows to determine with sufficient accuracy aerodynamic coefficients, necessary for diagnosis of available aeronautical engineering and for prediction of new real speciments</span&...
| Main Authors: | , , , |
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| Format: | Article |
| Language: | English |
| Published: |
National Aviation University
2000-09-01
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| Series: | Vìsnik Nacìonalʹnogo Avìacìjnogo Unìversitetu |
| Online Access: | http://jrnl.nau.edu.ua/index.php/visnik/article/view/9769 |