Improved estimation of air-to-air missile aerodynamic characteristics with using CFD Method

Result code in IS VaVaI
<a href="https://www.isvavai.cz/riv?ss=detail&h=RIV%2F60162694%3AG43__%2F20%3A00555372" target="_blank" >RIV/60162694:G43__/20:00555372 - isvavai.cz</a>
Result on the web
<a href="http://aimt.cz/index.php/aimt/article/view/1327" target="_blank" >http://aimt.cz/index.php/aimt/article/view/1327</a>
DOI - Digital Object Identifier
<a href="http://dx.doi.org/10.3849/aimt.01327" target="_blank" >10.3849/aimt.01327</a>

Result language
angličtina
Original language name
Improved estimation of air-to-air missile aerodynamic characteristics with using CFD Method
Original language description
Paper describes a solving procedure of the special Finite Volume Method (FVM) problem dealing with calculation of a flow field around air-to-air missile at subsonic, transonic and supersonic velocity range in order to obtain a coefficient of drag (CD). Some emphasis is put on numerical solution and fundamentals of FVM and use of a k-ω turbulence model for simulation of subsonic and supersonic flow fields around air-to-air missile AIM-9 Sidewinder version M. Obtained results of missile aerodynamics characteristics are verified using semi-empirical software and by analysis of flow fields.
Czech name
—
Czech description
—

Type
J<sub>SC</sub> - Article in a specialist periodical, which is included in the SCOPUS database
CEP classification
—
OECD FORD branch
20302 - Applied mechanics

Project
—
Continuities
I - Institucionalni podpora na dlouhodoby koncepcni rozvoj vyzkumne organizace

Publication year
2020
Confidentiality
S - Úplné a pravdivé údaje o projektu nepodléhají ochraně podle zvláštních právních předpisů

Similar results(10)