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

Year: 2025

Type: article

Abstract: This paper presents a historical review of key mathematical models and the evolution of direct, inverse, and mixed methods for designing high-lift profiles featuring surface air suction and blowing through slotted nozzles. It traces the development of approaches to solving inverse ill-posed boundary value problems in aerodynamics. Inverse ill-posed methods for designing aerodynamic profiles are discussed in the context of developing transport aircraft with a lifting propulsive fuselage and low-aspect-ratio wings.

Source: Aèrokosmičeskaâ tehnika i tehnologii.

DOI: 10.52467/2949-401x-2025-3-2-226-260

Authors: P. V. Bulat, S. Yu. Dudnikov, N. V. Prodan, P. S. Chernyshov

Institutions: Baltic State Technical University Voenmeh, Sevastopol State University

Language: English

Topic: Computational Fluid Dynamics and Aerodynamics

Subfield: Computational Mechanics

Field: Engineering

Domain: Physical Sciences

Open Access status: hybrid

OpenAlex ID: W4414133052

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