Bending vibrations of a thin wing for a profile with two axes of symmetry

• Autorzy: Thao Hoang Thi Minh , Thanh Le Thi

Identyfikatory

DOI

10.59441/ijame/194850

• Języki publikacji: EN

Abstrakty

EN

In this work, we study the bending vibrations of a thin wing for a profile with two axes of symmetry, taking into account the influence of torsional vibrations on them. The primary focus of the current study is on finding an analytic solution for the wing-bending equation through the Laplace transform, determining the frequency of free-bending vibrations, and constructing the amplitude-frequency response and phase-frequency response of the wing.

Słowa kluczowe

EN

torsional vibrations; bending vibrations; airfoil with two axes of symmetry; Mach number; natural frequencies

PL

drgania skrętne; profil lotniczy; liczba Macha; częstotliwości własne

• Wydawca: Oficyna Wydawnicza Uniwersytetu Zielonogórskiego
• Czasopismo: International Journal of Applied Mechanics and Engineering
• Rocznik: 2024
• Tom: Vol. 29, no. 4
• Strony: 106--120
• Opis fizyczny: Bibliogr. 19 poz., tab., wykr.

Twórcy

autor

Thao Hoang Thi Minh

• Department of Mathematics, Faculty of Applied Sciences, Ho Chi Minh City University of Technology and Education, Ho Chi Minh City, VIETNAM

autor

Thanh Le Thi

• Department of Mathematics, Faculty of Applied Sciences, Ho Chi Minh City University of Technology and Education, Ho Chi Minh City, VIETNAM

• https://orcid.org/0000-0003-2191-8868

Bibliografia

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Uwagi

Opracowanie rekordu ze środków MNiSW, umowa nr POPUL/SP/0154/2024/02 w ramach programu "Społeczna odpowiedzialność nauki II" - moduł: Popularyzacja nauki (2025)