Dynamic instability of composite sandwich joined conical–cylindrical shell interacting with supersonic gas stream
B. Uspensky
Anatolii Pidhornyi Institute of Power Machines and Systems of National Academy of Science of Ukraine, Kharkiv, Ukraine
Search for more papers by this authorCorresponding Author
K. Avramov
Anatolii Pidhornyi Institute of Power Machines and Systems of National Academy of Science of Ukraine, Kharkiv, Ukraine
Department of Aircraft Strength, National Aerospace University N. Ye. Zhukovsky “KhAI”, Kharkiv, Ukraine
Kharkiv National University of Radio Electronics, Kharkiv, Ukraine
Correspondence
K. Avramov, Anatolii Pidhornyi Institute of Power Machines and Systems of National Academy of Science of Ukraine, Kharkiv, Ukraine.
Email: [email protected]
Search for more papers by this authorA. Salenko
National Technical University of Ukraine “Igor Sikorsky Kyiv Polytechnic Institute”, Kiev, Ukraine
Search for more papers by this authorO. Nikonov
Kyiv National University of Technologies and Design, Kyiv, Ukraine
Search for more papers by this authorB. Uspensky
Anatolii Pidhornyi Institute of Power Machines and Systems of National Academy of Science of Ukraine, Kharkiv, Ukraine
Search for more papers by this authorCorresponding Author
K. Avramov
Anatolii Pidhornyi Institute of Power Machines and Systems of National Academy of Science of Ukraine, Kharkiv, Ukraine
Department of Aircraft Strength, National Aerospace University N. Ye. Zhukovsky “KhAI”, Kharkiv, Ukraine
Kharkiv National University of Radio Electronics, Kharkiv, Ukraine
Correspondence
K. Avramov, Anatolii Pidhornyi Institute of Power Machines and Systems of National Academy of Science of Ukraine, Kharkiv, Ukraine.
Email: [email protected]
Search for more papers by this authorA. Salenko
National Technical University of Ukraine “Igor Sikorsky Kyiv Polytechnic Institute”, Kiev, Ukraine
Search for more papers by this authorO. Nikonov
Kyiv National University of Technologies and Design, Kyiv, Ukraine
Search for more papers by this authorAbstract
The dynamic instability of composite sandwich joined conical–cylindrical thin-walled structure interacting with the supersonic gas stream is studied. The motions of every layer are described by five variables: three displacement projections and two rotation angles of normal to layer middle surfaces. The piston theory is used to describe a supersonic gas stream interacting with a thin-walled structure. Using the assumed-mode method, the system of ordinary differential equations with respect to generalized coordinates is derived to describe the structure dynamics. The characteristic exponents are calculated to obtain the regions of dynamic instability on the system parametric planes. Numerical analysis is performed for composite thin-walled structure with face layers, which are manufactured from carbon fiber-reinforced composite. The honeycomb core of the thin-walled structure is additively manufactured from ULTEM material. The properties of dynamical instability regions of the joined conical–cylindrical shell are studied numerically.
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