Pages that link to "Item:Q2092914"
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The following pages link to Aerothermoelastic analysis of curvilinear fiber variable stiffness laminated panels in supersonic flow (Q2092914):
Displaying 10 items.
- Aerothermoelastic analysis of lattice sandwich composite panels in supersonic airflow (Q296080) (← links)
- Parametric study on supersonic flutter of angle-ply laminated plates using shear deformable finite element method (Q362962) (← links)
- A parametric study on supersonic/hypersonic flutter behavior of aero-thermo-elastic geometrically imperfect curved skin panel (Q645329) (← links)
- Nonlinear aero-thermal flutter postponement of supersonic laminated composite beams with shape memory alloys (Q1658026) (← links)
- Panel flutter analysis of cracked functionally graded plates in yawed supersonic flow with thermal effects (Q2240374) (← links)
- Aerothermoelastic analysis of panel flutter based on the absolute nodal coordinate formulation (Q2340351) (← links)
- Meshless analysis for modal properties and stochastic responses of heated laminated rectangular/sectorial plates in supersonic airflow (Q2691038) (← links)
- Thermo-mechanical design aspects for primary composite structures of large transport aircraft (Q2720346) (← links)
- Snap-through response of three-dimensional braided composite panels in thermal-acoustic-aero coupled field (Q6049500) (← links)
- Numerical investigation of aerothermoelastic characteristics of a thin heated panel in high supersonic and hypersonic flow (Q6157757) (← links)