Synonyme wurden verwendet für:
Flugmechanik
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keywords:("Flugmechanik")
Application of time-domain unsteady aerodynamics to rotary-wing aeroelasticity
Vibration analysis of composite turbopropellers using a nonlinear beam-type finite-element approach
Die Anwendbarkeit einfacher Hubschraubermodelle für flugmechanische Untersuchungen
The effect of airframe aerodynamics on V-22 rotor loads
Digital simulation of a 6-DOF multi-body dispense with body-on-body collision detection
Time and frequency-domain identification and verification of BO 105 dynamic models
Validation of mathematical simulations of helicopter vertical response characteristics in hover
Hingeless rotor aeroelastic stability analysis with refined aerodynamic modeling
Blade response calcultaions using three-dimensional aerodynamic modeling
Rotor design optimization using a multidisciplinary approach
Aeromechanical stability of a bearingless composite rotor in forward flight
An unsteady airload model with dynamic stall for rotorcraft simulation
Prediction of rotor aeroacustic in forward flight by a lifting surface method
Simulating moth wing aerodynamics: Towards the development of flapping-wing technology
Nutzung des A340-Simulators für Flugeigenschaftsanalysen
Methode zur technisch-wirtschaftlichen Bewertung von Drehflügler-Entwürfen in der Konzeptphase
Method for identification of non-linear multi-degree-of-freedom systems
Synthese und Analyse im parametrischen Flugzeugvorentwurf
Dynamic analysis of flexible supercavitating vehicles using modal based elements
Complex configuration meshing - an industrial view and approach
Optimization of asymmetric oblique flying wing configurations under variable constraints
Incorporation of aircraft performance considerations in inverse airfoil design
Higher order staggered coupling schemes to predict the aeroelastic behavior of helicopter rotors
Optimization of rotorcraft flight following engine failure
A parametric design study for a swashplateless helicopter rotor with trailing-edge flaps
Micro-rotorcraft performance improvement using trailing-edge gurney flaps
State-space representation of vortex wakes by the method of lines
Optimization of critical trajectories for rotorcraft vehicles
Hybridmodellierung und Systemidentifizierung der nichtlinearen Hubschrauber-Flugdynamik
Lagerloses aktives Rotorsystem. LARS. Abschlussbericht. Berichtszeitraum: 01.07.2003 - 31.12.2005
Development of an attitude guidance and control system for the Thunderstar suborbital spacecraft
Methode zur Prognose des Einflusses von Flugzeugsystemen auf die Missionskraftstoffmasse