Dynamic behavior of the vortex ring formed on a butterfly wing
Application of time-domain unsteady aerodynamics to rotary-wing aeroelasticity
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
DGLR-Fachgruppe 4 "Flugmechanik und Flugfuehrung" Taetigkeit der Fachausschuesse 1972, Koeln
Experimental investigation of hypersonic buzz on a delta configuration
Oppertunities in flight/propulsion control coupling (FPCC)
Guidance and control of a spacecraft to rendezvous and dock with a non-cooperative target
Effects of a spin chute installation on spin characteristics
Beiträge zum Verhalten von Raketennutzlastkörpern beim atmosphärischen Wiedereintritt
The effect of simulator motion on pilot control behaviour for agile and inert helicopter dynamics
Mathematical modelling of a helicopter rotor track and balance: Theory
Aerodynamics and Structural Mechanics of Flapping Flight with Elastic and Stiff Wings
Einfluss verschiedener Steigmethoden ausserhalb der Kaiser-Kurve auf die Steigzeit
Air-bearing facility for the simulation of spin-stabilized satellites
A theoretical technique for analyzing aeroelastic stability of bearingless rotors
Modelling the aerodynamics of coaxial helicopters - from an isolated rotor to a complete aircraft
Investigation on rotor blade-wake interaction noise in descent flight conditions
Rotor aerodyanmic in ground effect at low advance ratios
Rotorcraft handling qualities engineering: Managing the tension between safety and performance
Development of an integrated propulsion control system
A review of rotorcraft wake modeling methods for flight dynamics applications
Genetic optimizations of EC-135 noise abatement flight procedures using an aeroacoustic database
Eine Methode zur Analyse der Dynamik von räumlichen Landeklappenmechanismen in Fehlerfällen
Experimental and numerical aspects of simulating unsteady flows around the X-31 configuration
Technische Entwicklung von Bodeneffektfahrzeugen TEBEFPhase 2
Equilibrium motion of unbalanced dual-spin spacecraft
Compound Helicopter Optimum Design Based on Genetic Algorithm
Performance improvement with variable rotor span and RPM
Friedliche Drohne. Flugversuchsträger mit Embedded-PC-Steuerung