Accession Number : ADA324125
Title : Effect of the Leading-Edge Extension (LEX) Fence on the Vortex Structure over the F/A-18.
Descriptive Note : Technical rept.,
Corporate Author : DEFENCE SCIENCE AND TECHNOLOGY ORGANIZATION CANBERRA (AUSTRALIA)
Personal Author(s) : Thompson, D. H.
PDF Url : ADA324125
Report Date : FEB 1997
Pagination or Media Count : 64
Abstract : The effects of the Leading Edge Extension (LEX) fence on the vortex structure over the F/A-18 at moderate to high angles of attack were studied using a 1/9 scale wind tunnel model and a 1/48 scale water tunnel model. Measurements at the tip of one of the vertical fins of the wind tunnel model confirmed that the fence reduced fin vibration caused by vortex breakdown. Flow visualisation in the water tunnel and in the wind tunnel showed that the fence caused the formation of a second LEX vortex, of the same sense as the main LEX vortex, but originating on the LEX leading edge outboard of the fence. Visualisation of the surface flow around the fence showed in detail how the fence caused the second LEX vortex. The effects on vortex breakdown and fin vibration of the interaction between the main and second LEX vortices are discussed.
Descriptors : *VORTICES, *LEADING EDGES, *FENCES, FIGHTER AIRCRAFT, VIBRATION, ANGLE OF ATTACK, FLOW VISUALIZATION, REDUCTION, SURFACES, FLOW FIELDS, VERTICAL ORIENTATION, ATTACK AIRCRAFT, VISUAL INSPECTION, AUSTRALIA, WIND TUNNELS, FINS, WIND TUNNEL MODELS, HIGH ANGLES, WATER TUNNELS.
Subject Categories : Military Aircraft Operations
Distribution Statement : APPROVED FOR PUBLIC RELEASE