A multi-fidelity workflow to derive physics-based conceptual design methods
A multi-fidelity workflow to derive physics-based conceptual design methods
Parametric design of aircraft geometry using partial differential equations
Miles' Equation in Random Vibrations : Theory and Applications in Spacecraft Structures Design
Thrust enhancement via gel-type liquid confinement of laser ablation of solid metal propellant
COOREFLEX-Turbo : Vorhaben-Nr. 1.3.1b : "Robustes Aero Design" : Abschlussbericht
COOREFLEX-Turbo : Vorhaben-Nr. 1.3.1b : "Robustes Aero Design" : Abschlussbericht