Pages that link to "Item:Q4929505"
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The following pages link to Coupled thermal, structural and vibrational analysis of a hypersonic engine for flight test (Q4929505):
Displaying 4 items.
- Deviation analysis of loosely coupled quasi-static method for fluid-thermal interaction in hypersonic flows (Q1648252) (← links)
- Fluid-thermal-structural coupled analysis of a radial inflow micro gas turbine using computational fluid dynamics and computational solid mechanics (Q1718835) (← links)
- Use of Energy-State Analysis on a Generic Air-Breathing Hypersonic Vehicle (Q3843049) (← links)
- Nonlinear aerothermoelastic analysis of deployable control fin with actuator stiffness subjected to high-speed compressible flows (Q6661901) (← links)