Quantifying Uncertainty Across Fidelity Levels in the Design of Aerospace Systems
Test elektrischer Antriebe für Hybridfahrzeuge mittels Hardware-in-the-Loop Simulation
A DISCRETE ADJOINT FRAMEWORK FOR LOW-BOOM SUPERSONIC AIRCRAFT SHAPE OPTIMIZATION (AIAA 2017-3326)
Das hohe Schutzniveau eines Pre-Crash Rückhaltesystems und seine breitbandige Wirkung
Impact of short- to medium-haul aircraft block time changes on airline yields
Impact of short- to medium-haul aircraft block time changes on airline yields
Challenges for Verifying and Validating Scientific Software in Computational Materials Science
Discrete adjoint approach for modeling unsteady aerodynamic design sensitivities
Entwicklung und Inbetriebnahme des ersten Fahrsimulators an der Hochschule Regensburg