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Flugmechanik
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Cost/performance benefits of large-scale ground vibration test systems
Control mechanism strategies for spin-stabilized projectiles
Conceptual design of a medium-sized joined-wing aircraft
Computational aerodynamics analysis of a Martian rotorcraft
Cell-vertex, multigrid Euler scheme for use with multiblock grids
Body-wing interference at supersonic speeds -- 1
Blade response calcultaions using three-dimensional aerodynamic modeling
A variable stability projectile using an internal moving mass
A theoretical technique for analyzing aeroelastic stability of bearingless rotors
A severity analysis for rotorcraft encounters with vortex wakes
A rational approach to comparing the performance of coaxial and conventional rotors
A quasilinear analysis and design technique for nonlinear flight control system
Application of time-domain unsteady aerodynamics to rotary-wing aeroelasticity
Application of Mathieu functions in theory of subsonic compressible flow past oscillating airfoils