Effect of Aerodynamic Configuration Parameters on Lateral-Directional Stability of Double-Swept Flying Wing Aircraft
Poor lateral-directional stability due to the absence of vertical stabilizer is a great risk to the aircraft with a flying wing layout. In this paper, an unmanned aerial vehicle with this kind of configuration is chosen as the research object. A three-dimensional model of the unmanned aerial vehicle is established, and then the sensitivity analysis is performed to obtain the effects of main aerodynamic shape parameters on lateral-directional flying quality. The results show that the roll mode and spiral mode of the aircraft meets the requirements of Level 1 flying quality in MIL-F-8785C. But t... Mehr ...
Verfasser: | |
---|---|
Dokumenttyp: | Artikel |
Erscheinungsdatum: | 2019 |
Reihe/Periodikum: | Journal of Aerospace Technology and Management, Vol 11, Iss 1, Pp 3919-3919 (2019) |
Verlag/Hrsg.: |
Instituto de Aeronáutica e Espaço (IAE)
|
Schlagwörter: | Dynamic stability / Flying wing / Sensitivity analysis / Dutch roll mode / Technology / T / Motor vehicles. Aeronautics. Astronautics / TL1-4050 |
Sprache: | Englisch |
Permalink: | https://search.fid-benelux.de/Record/base-27016741 |
Datenquelle: | BASE; Originalkatalog |
Powered By: | BASE |
Link(s) : | https://doi.org/10.5028/jatm.v11.1074 |