Heat transfer with interface effects in high-enthalpy and high-speed flow: Modelling review and recent progress
X Yang, G **ao, Y Du, L Liu, D Wei, Y Gui - Applied Thermal Engineering, 2021 - Elsevier
Aerodynamics, aerothermodynamics and thermal protection system response in high-
enthalpy and high-speed flow is heat transfer with interface effects in nature. Modelling and …
enthalpy and high-speed flow is heat transfer with interface effects in nature. Modelling and …
Aeroelastic and aerothermoelastic analysis in hypersonic flow: past, present, and future
HYPERSONIC flight began in February 1949 when a WAC Corporal rocket was ignited from
a US-captured V-2 rocket [1]. In the six decades since this milestone, there have been …
a US-captured V-2 rocket [1]. In the six decades since this milestone, there have been …
Studies on fluid-thermal-structural coupling for aerothermoelasticity in hypersonic flow
AJ Culler, JJ McNamara - AIAA journal, 2010 - arc.aiaa.org
CURRENTLY, there is a focus by NASA and the US Department of Defense on the
development of hypersonic technologies for next-generation reusable launch vehicles and …
development of hypersonic technologies for next-generation reusable launch vehicles and …
A review of nonlinear aero-thermo-elasticity of functionally graded panels
Functionally Graded Materials (FGM) have attracted significant interest as heat-shielding
materials for space vehicle, skin sub-structures, gas turbine blades technologies, and many …
materials for space vehicle, skin sub-structures, gas turbine blades technologies, and many …
Reduced-order aerothermoelastic framework for hypersonic vehicle control simulation
DESIGN and simulation of hypersonic vehicle (HSV) control systems requires consideration
of a variety of disciplines due to the highly coupled nature of the flight regime [1–4]. To …
of a variety of disciplines due to the highly coupled nature of the flight regime [1–4]. To …
Approximate modeling of unsteady aerodynamics for hypersonic aeroelasticity
HISTORICALLY, the development of airbreathing hypersonic vehicles has encountered
difficulties due in part to the inability to survive the extreme temperatures associated with …
difficulties due in part to the inability to survive the extreme temperatures associated with …
Mitigating aeroelastic vibration of strongly nonlinear metamaterial supersonic wings under high temperature
Reducing aeroelastic vibration of supersonic aircraft wings is very challenging because of
the limitation of efficiency, mass, space and especially the extreme high and variable …
the limitation of efficiency, mass, space and especially the extreme high and variable …
Correlation of supersonic wind tunnel measurements with a nonlinear aeroelastic theoretical/computational model of a thin plate
Supersonic wind tunnel test data is compared with a nonlinear aeroelastic computational
model, considering a freestream flow with Mach nearly 2, coupled cavity, and no-shock …
model, considering a freestream flow with Mach nearly 2, coupled cavity, and no-shock …
Model reduction of computational aerothermodynamics for hypersonic aerothermoelasticity
AR Crowell, JJ McNamara - AIAA journal, 2012 - arc.aiaa.org
CURRENTLY, there is a need for improved access to space using next generation, air-
breathing-based reusable launch technologies, such as that illustrated in Fig. 1. As a result …
breathing-based reusable launch technologies, such as that illustrated in Fig. 1. As a result …
Axially functionally graded beams and panels in supersonic airflow and their excellent capability for passive flutter suppression
Z Song, Y Chen, Z Li, J Sha, F Li - Aerospace Science and Technology, 2019 - Elsevier
Mode localization in the airflow direction can be observed in aeroelastic structures. On the
contrary, can the aeroelastic stability of the structure be enhanced if the geometric sizes and …
contrary, can the aeroelastic stability of the structure be enhanced if the geometric sizes and …