Pages that link to "Item:Q4447018"
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The following pages link to Steady/unsteady aerodynamic analysis of wings at subsonic, sonic and supersonic Mach numbers using a 3D panel method (Q4447018):
Displaying 3 items.
- An improved kernel function computation in subsonic unsteady lifting surface theory (Q1064888) (← links)
- Behaviour of a rectangular wing in a supersonic flow-dynamic pressure and normal force analysis in the range 1.3-4.0 mach (Q1065639) (← links)
- Supersonic flutter analysis of wings using an unsteady 3D panel method (Q5929811) (← links)