Methode zur Prognose des Einflusses von Flugzeugsystemen auf die Missionskraftstoffmasse
Methode zur technisch-wirtschaftlichen Bewertung von Drehflügler-Entwürfen in der Konzeptphase
Method for identification of non-linear multi-degree-of-freedom systems
Metody rešenija mnogokriterial'nych zadač sinteza techničeskich sistem
Micro-rotorcraft performance improvement using trailing-edge gurney flaps
Modeling lead-lag dynamics for rotorcraft-pilot-couplings investigation
Modelling the aerodynamics of coaxial helicopters - from an isolated rotor to a complete aircraft
Modern wind tunnel techniques for unsteady testing - development of dynamic test rigs
Numerical methods for the aeromechanical design of flapping wing hovering MAV
Nutzung des A340-Simulators für Flugeigenschaftsanalysen
Oppertunities in flight/propulsion control coupling (FPCC)
Optimal approach minimizing aircraft noise and fuel consumption
Optimal control : workshop, Universität Greifswald, 1.-3. Oktober 2002
Optimal penetration landing trajectories in the presence of windshear
Optimization of asymmetric oblique flying wing configurations under variable constraints
Optimization of critical trajectories for rotorcraft vehicles
Optimization of rotorcraft flight following engine failure
Parallel computing of helicopter response to turbulence toward real-time implementation
Performance analysis of the slowed-rotor compound helicopter configuration
Performance improvement with variable rotor span and RPM
Performance of a cycloidal rotor concept for micro air vehicle applications
Performance, stability, dynamics, and control of airplanes
Performance, stability, dynamics, and control of airplanes
Physik des Fliegens, Strömungsphysik, Raketen, Satelliten
Praktische Aerodynamik für Flugzeuge mit Strahltriebwerken
Prediction of rotor aeroacustic in forward flight by a lifting surface method
Preliminary Design of a Mach 6 Configuration Using MDO
Proceedings of NPU/AIAA Atmospheric Flight Mechanics Conference : Xian, June 11 - 14, 1996