Determination of Vortex Paths by Series Expansion Technique with Application to Cruciform Wings

A series method of determining two-dimensional vortex paths is considered and applied to the computation of vortex positions behind a slender equal-span cruciform wing at any angle of bank as a function of the distance behind the trailing edge. Calculated paths are shown for four bank angles. For a...

Ausführliche Beschreibung

Bibliographische Detailangaben

1. Verfasser:	Alksne, Alberta Y
Format:	Report
Sprache:	eng
Schlagworte:	Aircraft AQ M00-08-2314 CRUCIFORM WINGS EXPANSION Guided Missiles INCOMPRESSIBLE FLOW SERIES(MATHEMATICS) TAIL ASSEMBLIES TRAILING EDGES VORTICES
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