Shear properties of a honeycomb structure with zero Poisson’s ratio

• Autorzy: Song L. , Sun Y. , Han Z. , Wang T. , Wang H. , Yin C. , Shen X.

Identyfikatory

DOI

10.24423/aom.4232

• Języki publikacji: EN

Abstrakty

EN

Honeycomb structures with zero Poisson’s ratio show promising potential for application in variable-sweep wing aircraft. The shear properties of these honeycomb structures serve as a crucial indicator of their morphing capacity. This paper derives the linear and non-linear shear properties of a honeycomb structure with zero Poisson’s ratio. A modified factor is introduced to establish a relationship between the linear and non-linear shear modulus of the honeycomb structure, simplifying the calculation method of the non-linear shear modulus. The validity of theoretical predictions is then confirmed using the finite element method Furthermore, the influences of the geometric parameters on the shear properties of the honeycomb structure with zero Poisson’s ratio are investigated, highlighting the varying contributions of these cell geometric parameters to the shear properties.

Słowa kluczowe

EN

honeycomb structure; zero Poisson’s ratio; shear properties; small deformation; large deformation

• Wydawca: Instytut Podstawowych Problemów Techniki PAN
• Czasopismo: Archives of Mechanics
• Rocznik: 2023
• Tom: Vol. 75, nr 5
• Strony: 521--541
• Opis fizyczny: Bibliogr. 33 poz., rys., wykr.

Twórcy

autor

Song L.

• State Key Laboratory of Mechanics and Control of Mechanical Structures, Nanjing University of Aeronautics and Astronautics, Nanjing, 210016, China

autor

Sun Y.

• Beijing Institute of Space Long March Vehicle, Beijing, 100076, China

autor

Han Z.

• Beijing Institute of Space Long March Vehicle, Beijing, 100076, China

autor

Wang T.

• State Key Laboratory of Mechanics and Control of Mechanical Structures, Nanjing University of Aeronautics and Astronautics, Nanjing, 210016, China

autor

Wang H.

• State Key Laboratory of Mechanics and Control of Mechanical Structures, Nanjing University of Aeronautics and Astronautics, Nanjing, 210016, China

autor

Yin C.

• State Key Laboratory of Mechanics and Control of Mechanical Structures, Nanjing University of Aeronautics and Astronautics, Nanjing, 210016, China

autor

Shen X.

• State Key Laboratory of Mechanics and Control of Mechanical Structures, Nanjing University of Aeronautics and Astronautics, Nanjing, 210016, China

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