Experimental Investigation of the Flowfield About an Upswept Afterbody

Experimental Investigation of the Flowfield About an Upswept Afterbody

The flowfield about the aft portion of an aircraft feuslage using an upswept afterbody is complex and can have a detailed vortex structure. Directional pressure probe measurements show that the afterbody wake evolution is weakly dependent on the Reynolds number.

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Veröffentlicht in:Journal of aircraft 1994-11, Vol.31 (6), p.1281
Hauptverfasser: Epstein, Ronald J, Carbonaro, Mario C, Caudron, F
Format: Artikel
Sprache:eng
Schlagworte:
Aircraft
Mechanical engineering
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Beschreibung
Zusammenfassung:The flowfield about the aft portion of an aircraft feuslage using an upswept afterbody is complex and can have a detailed vortex structure. Directional pressure probe measurements show that the afterbody wake evolution is weakly dependent on the Reynolds number.
ISSN:0021-8669
1533-3868
DOI:10.2514/3.46648