COMPUTER MODEL OF AN AIRCRAFT TURBULENT FLOW OVER AND CALCULATION OF IT’S AERODYNAMIC CHARACTERISTICS
The original semiempirical model of turbulent flow of air in an interface of an aircraft surface is described in this work. Based on this model the computer system allowing to simulate aerodynamic processes around an aircraft and to calculate it’s aerodynamic characteristics was developed. These cha...
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| Veröffentlicht in: | Sistemnyĭ analiz i prikladnai͡a︡ informatika. 2015-08 (1), p.41-46 |
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| Hauptverfasser: | , |
| Format: | Artikel |
| Sprache: | eng |
| Online-Zugang: | Volltext |
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| Zusammenfassung: | The original semiempirical model of turbulent flow of air in an interface of an aircraft surface is described in this work. Based on this model the computer system allowing to simulate aerodynamic processes around an aircraft and to calculate it’s aerodynamic characteristics was developed. These characteristics are used by aircraft designers for an assessment of quality and properties of an aircraft. |
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| ISSN: | 2309-4923 2414-0481 |