High performance gas transmission compressor cylinders
Comparison of simulation and flight-test data for missile systems
Complex system modelling with fault trees and stochastic processes
MEDUSA - ein Mehrkoerperprogramm zur Analyse und Auslegung der Dynamik von spurgefuehrten Fahrzeugen
Mission effectiveness model for a system with several mission types
Space-harmonic and end-transient representations of the linear induction motor
A three-dimensional, block-structured finite element grid generation scheme
Zulaessige Schwingbeanspruchungen fuer elektrische Generatoren, Teil 2
Acoustic finite elements and their industrial applications
Boundary element analysis of linear induction motor for Maglev vehicle
Design of single-sided linear induction motors for urban transit
On damage tolerance design of fuselage structure - circumferential cracks
Response to changes in noise exposure: testin a model
The effectiveness of high intensity acoustic noise testing
The production of ground vibrations by railway trains
The effect of airframe aerodynamics on V-22 rotor loads
The manipulator development and simulation facility for space station robotics
A study of symbolic processing and computational aspects in helicopter dynamics
Correlation autoregressive processes with application to helicopter noise
An unsteady helicopter rotor-fuselage aerodynamic interaction analysis
Assessment of transient analysis techniques for rotor stability testing
Assembly of finite-element helicopter subsystems with large relative rotations
Investigation of variation in fatigue life calculated using damage fraction
An experimental and analytical investigation of isolated rotor flap-lag stability in forward flight
Helicopter response to atmospheric turbulence in forward flight
Tire structural parameter analysis for road noise using an accurate FEM model
A mathematical model to simulate small boat behaviour
Optimization of the sound pressure level pattern for a curved array sonar transducer
Neue Wege zur Untersuchung der Fahrweg-Fahrzeug-Dynamik. Teil 1
Use of eigenstructure assignment in VSTOL aircraft control law design
Effect of hingeless rotor aeroelasticity on helicopter longitudinal flight dynamics
Rotor loads prediction utilizing a coupled aeroelastic analysis with refined aerodynamic modeling