C
Chonghui Shao
Researcher at Harbin Institute of Technology
Publications - 9
Citations - 104
Chonghui Shao is an academic researcher from Harbin Institute of Technology. The author has contributed to research in topics: Flutter & Aeroelasticity. The author has an hindex of 4, co-authored 9 publications receiving 71 citations.
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Thermal-structural analysis for an attitude maneuvering flexible spacecraft under solar radiation
TL;DR: In this paper, a coupled thermal-structural analysis for an attitude maneuvering spacecraft under solar radiation is conducted and the interaction between the thermally induced vibration and attitude maneuver is studied.
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An admissible function for vibration and flutter studies of FG cylindrical shells with arbitrary edge conditions using characteristic orthogonal polynomials
TL;DR: In this article, a general approach for the vibration and aeroelastic stability of the functionally graded cylindrical shell with arbitrary boundary conditions is firstly presented, where the Sanders' shell theory, a steady-state heat transfer equation and the piston theory are employed to establish the motion equation.
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Studies for aeroelastic characteristics and nonlinear response of FG-CNT reinforced composite panel considering the transient heat conduction
TL;DR: In this paper, a solution of computing the aero-thermal-elastic problem of FG-CNT reinforced composite panel is proposed, in which the aerodynamic heating and transient heat conduction are accounted for.
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Flutter and Thermal Buckling Analysis for Composite Laminated Panel Embedded with Shape Memory Alloy Wires in Supersonic Flow
TL;DR: In this article, the flutter and thermal buckling behavior of laminated composite panels embedded with shape memory alloy (SMA) wires are investigated using the classical plate theory and nonlinear von-Karman strain-displacement relation to investigate the aeroelastic behavior of smart laminated panels.
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An alternative simulation approach for the ONERA aerodynamic model and its application in the nonlinear aeroelastic analysis of slender wings with pylon-store system
TL;DR: In this paper, an alternative simulation approach is proposed to simplify the calculations for the ONERA model, in which the circulatory part of the OnERA model is solved analytically by using Duhamel integral method, and the corresponding aerodynamic loads can be directly expressed in the modal space of the wing motion through only introducing two additional variables.