Computation of F/A-18 tail buffet

The aerodynamic loads that cause tail buffet on the F/A-18 fighter aircraft were analyzed using computational fluid dyanmics (CFD). The half-body aircraft geometry was modeled using an overset grid system.

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Bibliographische Detailangaben
Veröffentlicht in:	Journal of aircraft 1996-11, Vol.33 (6), p.1181-1189
Hauptverfasser:	Gee, Ken, Murman, Scott M, Schiff, Lewis B
Format:	Artikel
Sprache:	eng
Schlagworte:	Aerodynamics Aircraft Applied sciences Exact sciences and technology Fluid dynamics Ground, air and sea transportation, marine construction Miscellaneous transportation
Online-Zugang:	Volltext
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Beschreibung
Zusammenfassung:	The aerodynamic loads that cause tail buffet on the F/A-18 fighter aircraft were analyzed using computational fluid dyanmics (CFD). The half-body aircraft geometry was modeled using an overset grid system.
ISSN:	0021-8669 1533-3868
DOI:	10.2514/3.47073