The following pages link to (Q5844142):
Displaying 7 items.
- An efficient finite differences method for the computation of compressible, subsonic, unsteady flows past airfoils and panels (Q1692049) (← links)
- Theoretical study on the instability mechanism of flutter generated on a cantilevered flexible plate in three-dimensional uniform flow (Q2234576) (← links)
- Prediction of incidence effects on oscillating airfoil aerodynamics by a locally analytical method (Q3815688) (← links)
- Steady/unsteady aerodynamic analysis of wings at subsonic, sonic and supersonic Mach numbers using a 3D panel method (Q4447018) (← links)
- The general motion of the aeroplane (Q5842188) (← links)
- (Q5843714) (← links)
- (Q5844017) (← links)