Time and frequency-domain identification and verification of BO 105 dynamic models
Cell-vertex, multigrid Euler scheme for use with multiblock grids
Validation of mathematical simulations of helicopter vertical response characteristics in hover
Hingeless rotor aeroelastic stability analysis with refined aerodynamic modeling
Blade response calcultaions using three-dimensional aerodynamic modeling
Rotor design optimization using a multidisciplinary approach
Flugmechanik : moderne Flugzeugentwurfs- und Steuerungskonzepte
Flugmechanik : moderne Flugzeugentwurfs- und Steuerungskonzepte
Estimation of aircraft inertia characteristics from bifilar pendulum test data
X-31A flight flutter test excitation by control surfaces
Aeromechanical stability of a bearingless composite rotor in forward flight
Experimental aerodynamic and aeroacoustic investigation of a scaled tilt rotor in hover
Parallel computing of helicopter response to turbulence toward real-time implementation
An unsteady airload model with dynamic stall for rotorcraft simulation