Dynamic behavior of the vortex ring formed on a butterfly wing
Experimental method for studying gust effects on micro rotorcraft
Conflict resolution in autonomous operations area airspace
Application of a Coupling of Flight Mechanics and Aerodynamics to Predict the SHEFEX I Ascent Phase
Preliminary Design of a Mach 6 Configuration Using MDO
Experimental investigation of hypersonic buzz on a delta configuration
Mathematical modelling of a helicopter rotor track and balance: Theory
Guidance and control of a spacecraft to rendezvous and dock with a non-cooperative target
The effect of simulator motion on pilot control behaviour for agile and inert helicopter dynamics
Beiträge zum Verhalten von Raketennutzlastkörpern beim atmosphärischen Wiedereintritt
Aerodynamics and Structural Mechanics of Flapping Flight with Elastic and Stiff Wings
Investigation on rotor blade-wake interaction noise in descent flight conditions
Einfluss verschiedener Steigmethoden ausserhalb der Kaiser-Kurve auf die Steigzeit
Modelling the aerodynamics of coaxial helicopters - from an isolated rotor to a complete aircraft
A theoretical technique for analyzing aeroelastic stability of bearingless rotors
Rotor aerodyanmic in ground effect at low advance ratios
A review of rotorcraft wake modeling methods for flight dynamics applications
Rotorcraft handling qualities engineering: Managing the tension between safety and performance
Genetic optimizations of EC-135 noise abatement flight procedures using an aeroacoustic database
Eine Methode zur Analyse der Dynamik von räumlichen Landeklappenmechanismen in Fehlerfällen
Equilibrium motion of unbalanced dual-spin spacecraft
Performance improvement with variable rotor span and RPM
Rotor power reduction using multiple spanwise-segmented, optimally-actuated trailing-edge flaps
Simulations- und Flugversuche über Flugeigenschaften von Hyperschall-Flugzeugen
Mathematical modelling of a helicopter rotor track and balance: Results
A rational approach to comparing the performance of coaxial and conventional rotors
Optimal approach minimizing aircraft noise and fuel consumption
Experimentelle und numerische Bestimmung der dynamischen Derivative
Hybridmodellierung und Systemidentifizierung der nichtlinearen Hubschrauber-Flugdynamik
Influence of rotor wakes on helicopter aerodynamic behaviour
Flexible aircraft modelling for flight loads analysis of wake vortex encounters
Addressing today's aeromechanic questions by industrial answers