Pages that link to "Item:Q2421973"
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The following pages link to Aerothermoelastic flutter analysis of pre-twisted thin-walled rotating blades reinforced with functionally graded carbon nanotubes (Q2421973):
Displaying 10 items.
- Dynamics of advanced rotating blades made of functionally graded materials and operating in a high-temperature field (Q930417) (← links)
- Aeroelastic characteristics of functionally graded carbon nanotube-reinforced composite plates under a supersonic flow (Q1798593) (← links)
- Meshless numerical approach to flutter analysis of rotating pre-twisted nanocomposite blades subjected to supersonic airflow (Q1980179) (← links)
- Nonlinear dynamic responses of functionally graded graphene platelet reinforced composite cantilever rotating warping plate (Q2110827) (← links)
- Modeling large amplitude vibration of pretwisted hybrid composite blades containing CNTRC layers and matrix cracked FRC layers (Q2182999) (← links)
- Computationally efficient model for flow-induced instability of CNT reinforced functionally graded truncated conical curved panels subjected to axial compression (Q2309800) (← links)
- Modeling aerothermoelastic properties and active flutter control of nanocomposite cylindrical shells in supersonic airflow under thermal environments (Q2310026) (← links)
- Size-dependent vibration analysis of an axially moving sandwich beam with MR core and axially FGM faces layers in yawed supersonic airflow (Q2325818) (← links)
- Computation of aerothermoelastic properties and active flutter control of CNT reinforced functionally graded composite panels in supersonic airflow (Q2414632) (← links)
- 1/2 and 1/3 subharmonic resonance behaviors of a rotating FG-CNTRC beam with geometric imperfections (Q6639996) (← links)
