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Flugmechanik
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keywords:("Flugmechanik")
Wing with inflatable spars and rigid ribs
Visual Dependency Structure Matrix for Multidisciplinary Design Optimization Tradeoff Studies
Vibrations of the walls of a rectangular duct containing fluid flow
Vibrational genetic algorithm as a new concept in airfoil design
Very light airplane longitudinal dynamic stability analysis
Validation of comprehensive dynamics analysis predictions for a rotor in descending flight
Using the dynamic mesh method for genetically obtained wing structures
Unsteady wake measurements behind an airfoil and prediction of dynamic stall from the wake
Tunnel Gaussian Process Model for Learning Interpretable Flight’s Landing Parameters
Transonic airfoil design and optimisation by using vibrational genetic algorithm
Trajectory optimization for hypersonic boost-glide missile considering aeroheating
Torque Optimal Steering of Control Moment Gyroscopes for Agile Spacecraft
Time-Varying Model Identification of Flapping-Wing Vehicle Dynamics Using Flight Data
The University of Glasgow unmanned aerial vehicle system
The turbo fan aircraft minimum cost climb technique
The training rate of aircraft handling quality evaluation scale
The safety of shipborne helicopter operation
The influence of human factors on operational efficiency
The HIRM+ Flight Dynamics Model
The flutter analysis of an infinitely long orthotropic panel in a rectangular duct
The 2nd International Conference on Recent Advances in Space Technologies
Target-Based Guidance Method for Trajectories with Multiple Flybys
Subscale flight testing used in conceptual design
Study of Aerodynamics of Propulsive Helicopter Fuselage
String Stable Heterogeneous Aircraft in a Windy Environment
State Transition Tensors for Continuous-Thrust Control of Three-Body Relative Motion
Stability of the stationary motion of the airship
Solution to rotor blade erosion in sandy environments
Simulation of helicopter motion in unsteady conditions
Simple virtual attitude sensors for general aviation aircraft
Shape optimization of the airfoil comprising a cross flow fan
Separation control on a NACA 0015 airfoil using a 2D micro ZNMF jet
Sensor and control surface/actuator failure detection and isolation applied to F-16 flight dynamic
Selected aerodynamic design issues for the single-rotor remotely piloted helicopter
Rotor unsteady aerodynamics model using an efficient free-vortex method
Rotary wing UAV potential applications: an analytical study through a matrix method
Pressure relief for jet engines – Photon ’02
Platooning and Base Flaps for Drag Reduction of Trucks
Parameters determination for concept design of solar-powered, high-altitude long-endurance UAV
Pacelab software for preliminary design