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Flugmechanik
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A Concept for Credibility Assessment of Aircraft System Simulators
Adaptive sampling strategies for reduced-order modeling
Adaptive vortex generators based on active hybrid composites: from idea to flight test
Adaptive vortex generators based on active hybrid composites: from idea to flight test
Aerodynamic design optimization of a helicopter rotor blade-sleeve fairing
Aerodynamic design optimization of a helicopter rotor blade-sleeve fairing
Aerodynamic Parameter Estimation for a Morphing Unmanned Aerial Vehicle from Flight Tests
Aeroelastic behaviour of a wing with over-the-wing mounted UHBR engine
Aeroelastic tailoring of an NLF forward swept wing
Aeroelastic tailoring of an NLF forward swept wing
A hybrid multilevel approach for aeroelastic optimization of composite wing-box
A multi-body approach for modelling manoeuvring aeroelastic aircraft during preliminary design
Analysis of trimmable conditions for a civil aircraft with active high-lift system
Analysis of trimmable conditions for a civil aircraft with active high-lift system
An improved high-lift aerodynamic prediction method for transport aircraft
An improved high-lift aerodynamic prediction method for transport aircraft
A parametric design study for a swashplateless helicopter rotor with trailing-edge flaps
Application of time-domain unsteady aerodynamics to rotary-wing aeroelasticity
A trim problem formulation for maximum control authority using the Attainable Moment Set geometry
A two-element high-lift airfoil in disturbed flow conditions
A two-element high-lift airfoil in disturbed flow conditions
Autonomous Load Control and Transportation Using Multiple Quadrotors
A variable stability projectile using an internal moving mass
Blade response calcultaions using three-dimensional aerodynamic modeling
Code-to-Code Benchmark for Simulation Tools Based on the Unsteady Vortex-Lattice Method
Comparison and evaluation of blade element methods against RANS simulations and test data
Conceptual design analysis of a variable swept half-span wing of a supersonic business jet
Design, Selection, and Evaluation of Reinforcement Learning Single Agents for Ground Target Tracking
Development of an attitude guidance and control system for the Thunderstar suborbital spacecraft
Development of a quasi-linear parameter varying model for a tiltrotor aircraft
Dynamic modeling and fuzzy control for a small tiltrotor unmanned aerial vehicle
Effect of an active high-lift system failure during landing approaches
Effect of an active high-lift system failure during landing approaches
Engine integration based on multi-disciplinary optimisation technique
Engine integration based on multi-disciplinary optimisation technique
Existence of Probability Density Function for Norm of Finite-Dimensional Random Vector
Experimental investigation of generic ice block trajectories under freestream conditions
Experimental investigation of generic ice block trajectories under freestream conditions
Flap efficiency analysis for the SAGITTA diamond wing demonstrator configuration
Flap efficiency analysis for the SAGITTA diamond wing demonstrator configuration
Flight Control with Optimal Control Allocation Incorporating Structural Load Feedback