Aerodynamic Per f ormance o f Low-to-Moderate Aspect Ratio Wings at Low Reynolds Numbers
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This thesis presents wind tunnel results of wings of low-to-moderate aspect ratio (2≤\AR≤5) tested at low Reynolds numbers (40,000 to 160,000). All models tested had a chord length of 3~in and a wingspan of 7 to 17.5~in.
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