An application of finite Hilbert transforms in the derivation of a state space model for an aeroelastic system
Dynamic modelling of various aerolastic control systems (e.g., an airfoil) requires an application of Söhngen's inversion formula for finite Hilbert transforms. In order to justify the validity of the inversion formula it is shown that the circulation history must belong to a weighted \(L_ 2\) space.
scientific article; zbMATH DE number 4215531