Pages that link to "Item:Q6157757"
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The following pages link to Numerical investigation of aerothermoelastic characteristics of a thin heated panel in high supersonic and hypersonic flow (Q6157757):
Displaying 7 items.
- A parametric study on supersonic/hypersonic flutter behavior of aero-thermo-elastic geometrically imperfect curved skin panel (Q645329) (← links)
- Effect of Mach number and plate thickness on the flow field and heat transfer characteristics of supersonic turbulent flow over a flat plate at different thermal boundary conditions (Q2055440) (← links)
- Aeroelastic characteristics of inflatable reentry vehicle in transonic and supersonic regions (Q2129513) (← links)
- Coupled thermal, structural and vibrational analysis of a hypersonic engine for flight test (Q4929505) (← links)
- Numerical Modeling of Coupled Problems of External Aerothermodynamics and Internal Heat-and-Mass Transfer in High-Speed Vehicle Composite Constructions (Q5274961) (← links)
- Numerical study of steam flow on the low-pressure turbine under off-design conditions: a case study of the Neka steam power plant (Q6661875) (← links)
- Nonlinear aerothermoelastic analysis of deployable control fin with actuator stiffness subjected to high-speed compressible flows (Q6661901) (← links)
