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The inverse approach is computationally efficient in aerodynamic design as the desired target performance distribution is specified. However, it has some significant limitations that prevent it from achieving full efficiency. First, the iterative procedure should be repeated whenever the specified target distribution changes. Target distribution optimization can be performed to clarify the ambiguity in specifying this distribution, but several additional problems arise in this process such asarXiv:2108.08500v2 fatcat:5bwu32pdkzfbnf4xabr6d25nni