Analysis of the Flow Past a Shockless Lifting Airfoil in Design and Off-Design Conditions.
NATIONAL AERONAUTICAL ESTABLISHMENT OTTAWA (ONTARIO)
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A shockless lifting airfoil designed for shockless inviscid flow at transonic vleocity was tested at high Reynolds numbers in design and off-design conditions. The experimental results are compared against theoretical results, showing in general good agreement.
- Fluid Mechanics