Категория: Aeromechanics and durability

Study of the variable camber morphing wing parameters influence on aerodynamic performance

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DOI 10.51955/2312-1327_2025_2_

Sergey V. Skorobogatov

Dmitry A. Buturov

Abstract. This paper presents a study of the variable camber morphing wing parameters influence on aerodynamic performance. A comparison of traditional plain flaps and slats (nose flaps) with variable camber morphing wing elements was performed. Numerical simulations were conducted using the XFLR5 software suite implementing XFOIL algorithms. The analysis was performed for a wide range of configurations and conditions, including variations in the rotation axis (hinge) position of the high-lift devices along the wing chord, and a broad range of deployment and angle-of-attack values. The key factors influencing the effectiveness of morphing high-lift devices have been identified.

Keywords: aerodynamics, morphing wing, plain flap, nose flap, high-lift devices.

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Structural estimation of compressor and turbine rotor blades of aircraft gas-turbine engines

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UDC 004.588 BBK 74.5

Karavaev Ju. A., Hodackij S. A.

В статье приведена методика прочностного расчёта рабочих лопаток компрессоров и турбин авиационных ГТД с использованием программы FEMAP.

Рассмотрены допущения, принимаемые при расчёте. Последовательно рассмотрены этапы расчёта. Приведено изменение напряжений по перу лопатки.

Ключевые слова: статическая прочность, напряжения, расчёт.

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Comprehensive reliability assessment of aerodynamic characteristics computed with ANSYS for compound objects

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UDC 629.7.016 BBK 39.5

Vshivkov Y. F., Galushko E. A., Krivel’ S. M. 

The article presents the main assessment results of calculating reliability of aerodynamic characteristics of a support system near the underlying surface. The assessment is based on comparing the calculation results with the experimental data and the results obtained by other authors using alternative methods.

Key words: aerodynamic characteristics; a WIG vehicle.

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