The flow field associated with the formation of a mushroom shaped trailing edge stall cell on a low-aspect-ratio (AR = 4.0) wing was investigated in a series of low speed wind tunnel tests (Reynolds number based on 15.2 cm chord = 480,000). Flow field surveys of the separation bubble and wake of a partially stalled and fully stalled wing were completed using a hot-wire probe, a split-film probe, and a directional sensitive pressure probe. A new color video display technique was developed to display the flow field survey data. Photographs were obtained of surface oil flow patterns and smoke flow visualization
An experimental study of separated flow on a finite wing
Atmospheric Flight Mechanics Conference ; 1981 ; Albuquerque, NM
1981-08-01
Aufsatz (Konferenz)
Keine Angabe
Englisch
An experimental study of separated flow on a finite wing
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