Results indicating that unsteady aerodynamic loads derived under the assumption of simple harmonic motions executed by airfoil or wing can be extended to arbitrary motions are summarized. The generalized Theodorsen (1953) function referable to loads due to simple harmonic oscillations of a wing section in incompressible flow, the Laplace inversion integral for unsteady aerodynamic loads, calculations of root loci of aeroelastic loads, and analysis of generalized compressible transient airloads are discussed.
Unsteady aerodynamic modeling for arbitrary motions
AIAA Journal ; 15
1977-04-01
Sonstige
Keine Angabe
Englisch
Unsteady aerodynamic modeling for arbitrary motions
AIAA | 1977
|Unsteady Aerodynamic Modeling fo0r Arbitrary Motions
AIAA | 1977
|Unsteady aerodynamic modeling for arbitrary motions
AIAA | 1979
|