Comparison of Flow-Visualised Vortices with Computed Geometry Over Thin Delta Wings
Technical memorandum rept.
AERONAUTICAL RESEARCH LABS MELBOURNE (AUSTRALIA)
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The vortex flow patterns over thin delta wings were photographed during experiments in a vertical water tunnel making use of appropriate flow visualisation techniques. The flow geometry for these wings was also calculated using the VORSBA vortex flow computer program. A comparison is made between the calculated and experimental results and discrepancies between them are discussed. Keywords Australia, Computations, Potential flow, Incompressible inviscid vortex flow.