The development of high-lift systems is a major step in the design of modern aircraft and has a strong influence on the overall aircraft performance and cost. Many trade-offs must be considered, including performance, maximum lift, weight, cost, and noise. Today, the design and test of high-lift systems still requires many months of wind tunnel tests. Wind tunnel tests are costly and generally do not fully represent real flight conditions accurately — installation effects can influence the results, small-scale models cannot fully resolve all geometric details, and flight Reynolds and Mach numbers cannot be reproduced easily.
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