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Flugmechanik
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Studies in tilt-rotor VTOL aircraft aeroelasticity, volume 1
Computation of helicopter rotor wake geometry and its influence on rotor harmonic airloads
A study of the lift-to-drag ratio capability of caret wing waveriders.
Gust response and its alleviation for a hingeless helicopter rotor in cruising flight.
Higher harmonic blade pitch control : a system for helicopter vibration reduction
Experimental trim drag values for conventional and supercritical wings
Drag Reduction Obtained by the Addition of a Boattail to a Box Shaped Vehicle
Experimental investigation of vortices shed by various wing fin configurations
A task-oriented side force flight control system for the A-10 aircraft
Sailing vessel dynamics : investigations into aero-hydrodynamic coupling
Marine propeller blade tip flows
Determination of corrections to flow direction measurements obtained with a wing-tip mounted sensor
The Aerodynamic Optimization of Wings at Subsonic Speeds and the Influence of Wingtip Design
Robust integrated flight and aeroelastic control system design for a large transport aircraft
Mechanisms underlying chasing behaviour of male blowflies
Identification modeling and characteristics of miniature rotorcraft
Integrated flight loads modelling and analysis for flexible transport aircraft
Integrated flight loads modelling and analysis for flexible transport aircraft
Numerical Investigation of Unsteady Crosswind Aerodynamics for Ground Vehicles
Conflict resolution in autonomous operations area airspace
Guidance and control of a spacecraft to rendezvous and dock with a non-cooperative target
Flexible aircraft modelling for flight loads analysis of wake vortex encounters
Robust and efficient methods for aircraft trim simulations
Robust and efficient methods for aircraft trim simulations
Damping Effects of Drogue Parachutes on Orion Crew Module Dynamics
Design, Implementation and Testing of Advanced Control Laws for Fixed-wing UAVs
Real-time predictive motion planning for fixed-wing aerial vehicles
Certifiable L1 adaptive control for helicopters
Certifiable L1 adaptive control for helicopters
Redesign of the rotor head of the C30 autogyro
Path controller implementation for airborne wind energy systems
Flight dynamic stability prediction with a linear frequency domain method
Control of Hexacopter UAV by using Non Linear Instegraal Sliding Model Controller
Vertical landing flight envelope definition
Influence of flight control laws on structural sizing of commercial aircraft