Titel BA SA MA HW exp the kon Eintrag Integration of an Open Rotor Concept into an Existing Aircraft Design Environment 2024-11-07 Integration of a Composite Cycle Engine into an Existing Aircraft Design Environment 2024-11-07 Integration of a Propulsive Fuselage into an Existing Aircraft Design Environment 2024-11-07 Aeroelastic Evaluation of the Structural Concept for a Hydrogen Aircraft with a Dry Wing Configuration 2024-09-23 Werkstudent/Praktikumssemester - Advanced Design/ Future Projects / Aircraft Design (m/w/d) 2024-08-21 Thesis in the Field of Aerostructural Wing Design at Bauhaus Luftfahrt 2024-07-15 Untersuchungen zur langfristigen Entwicklung der Lärmimmissionen am Flughafen München 2024-07-12 Studentische Hilfskraft für das Praktikum "CAD im Flugzeugbau - CATIA V5" gesucht 2023-09-15 Implementation of an Aeroelastic Coupling Method for Flutter Simulation of Sailplanes 2022-04-28 Implementation of an Aerodynamic Solver for Aeroelastic Simulation of Sailplanes 2022-04-25 Aeroakustische Modellierung eines eVTOL UAVs 2021-10-25 Aerodynamische und aeroakustische Propellervalidierung 2021-10-25
