Vortex wake investigation behind a wing-flap model with jet simulations

To get a better insight in the effect of jets on vortex development and decay, stereo-PIV measurements were performed in a towing tank behind a flapped aircraft model. The experimental data set yields the wake vortex behavior in a range that extends from the vortex formation stage up to the mid-field (approximately t* =2 corresponding to 100...

The eN method for transition prediction: Historical review of work at TU Delft

Engineering primitives to reuse design process knowledge

Design tradeoffs for fiber composite fuselages under dynamic loads using structural optimization

Description and Flow Assessment of the Delft Hypersonic Ludwieg Tube

Domain specific modeling languages to support model-driven engineering of aircraft systems

Unsteady adaptive stochastic finite elements for aeroelastic systems with randomness