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Overview of the NASA 5.5 m composite cryotank technology development program
Comparison of modelled and actual car dynamic frontal crush
Hydroelastic viscous oscillations in a circular cylindrical container with an elastic cover
Antriebselemente - neue Werkstoffe für verbesserte Eigenschaften
Optimum design of submerged cylindrical shells subjected to dynamic loadings
Overview of Boeing's shape memory alloy based morphing aerostructure
Press performance, forming geometry and fracture behaviour in actual autobody panels
Boundary-layer-induced secondary flows on wing-body configurations
Active flow control on low-pressure turbine blades using synthetic jets
Current aerodynamic heating problems with first order shape change effects
Galling behaviour and its tests in press forming of autobody parts
Zweikomponentenstroemung im vertikalen Rohr bei der Foerderung von Eisen-Mangan-Konkretionen
Studies on twin non-parallel unventilated axisymmetric jets
Experimental modal analysis of an aeronautical engine component
Bistatic-radar estimation of surface-slope probability distributions with applications to the moon
Viscoplastic analysis of an experimental cylindrical thrust chamber liner
Elastic properties of Additive Manufacturing materials for automotive applications
An integrated circuit modular library for angle-based engine control
The trajectory of a projectile when fired parallel and near to the tree surface of a plastic solid
Some psychological tests of the conspicuities of emergency vehicle warning lights
Kinematic analysis of a novel rimless wheel with independently actuated spokes
Hydroforging of Thick-Walled Hollow Aluminum Profiles
A numerical study of dynamic buckling of thin-walled hollow square columns subjected to axial impact
Experimental analysis of propeller interactions with a flexible wing micro air vehicle
A refined analysis of sloshing effects in seismically excited tanks
Contrasting the Parasitic Torque on a Drag-Driven VAWT through a Variable-Blade Rotor Architecture
Schiebewinkeleinflüsse auf druckinduzierte laminare Ablöseblasen in dreidimensionalen Grenzschichten
Konstruieren, Berechnen, Erproben - Ingenieure nutzen die Moeglichkeiten moderner Computer-Technik
Gleichungen fuer die Bewegung eines Transportmittels in der Querebene
Aerodynamische Untersuchungen an Doppeldeltafluegeln bei unsymmetrischer Stroemung