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Development of the theory and methods for designing high-lift and propulsive profiles

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Designing high-lift profiles effectively improves aircraft performance and efficiency.
Key developments include the evolution of inverse ill-posed boundary value methods in aerodynamics.
Mathematical models provide essential frameworks for design methods using surface air suction.
Transport aircraft development benefits from tailored lifting propulsive fuselage and wing designs.

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Historical review highlights mathematical models and inverse ill-posed methods in aerodynamics.

Булат et al. (2025) studied this question.

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