Publication View

Effect of the Leading-Edge Extension (LEX) Fence on the Vortex Structure over the F/A-18. (1997)

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.

Publication details
Download http://handle.dtic.mil/100.2/ADA324125
Contributors DEFENCE SCIENCE AND TECHNOLOGY ORGANIZATION CANBERRA (AUSTRALIA)
Repository Defense Technical Information Center OAI-PMH Repository (United States)
Keywords MILITARY AIRCRAFT OPERATIONS, *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., LEX(LEADING EDGE EXTENSION), F/A-18 AIRCRAFT
Language eng