Tungsten-rhenium thick film thermocouples (TFTCs) show excellent potential for in-situ high-
temperature monitoring due to their high-temperature resistance. However, the only reported …

The main goal of this paper is to expand previously conducted study and consequently to
upgrade the proposed multimodular numerical framework developed for fluid–structure …

In this paper, a nonlinear aerothermoelastic analysis of a deployable control fin subjected to
Mach 7 hypersonic flow is presented. The fin consists of the inboard and outboard parts …

In the present work, fluid–thermal–structural interaction analyses of a thin pre-heated and
pre-buckled stiffened panel subjected to high-speed flow from Mach 3 to Mach 6 are …

The current work investigates the aerothermoelastic behavior of control fins with nonlinear
deployable joints connected to a nonlinear actuator. The fin is attached to a cylindrical body …

In the present work, nonlinear aerothermoelastic characteristics of a deployable control fin
subjected to high supersonic and hypersonic flow are investigated. The delayed detached …

In order to solve the problem of large rotating missile surface infrared radiation interference
during the dual-band infrared radiation attitude measurement and improve the infrared …

The thermo mechanical buckling and post-buckling behavior of layered composite shell type
structure are considered with the finite element method under the combination of …

In the flight process of a rudder wing structure in a hypersonic environment, a large
temperature gradient is generated due to severe aerodynamic heating, leading to structural …

Aiming at the influence of the aerodynamic heating effect of the high-speed vehicle on the
optical performance of the vehicle, the heat radiation model of the dome window of the …