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Mesh adaptation based on error estimation has become a key technique to improve the accuracy of computationalfluid-dynamics computations. The adjoint-based approach for error estimation is one of the most promising techniques for computational-fluid-dynamics applications. Nevertheless, the level of implementation of this technique in the aeronautical industrial environment is still low because it is a computationally expensive method. In the present investigation, a new mesh refinement methoddoi:10.2514/1.j051450 fatcat:4apo4kj5djcfvcpjhxsxnpnz5e