Aeroakustische Bewertung von Fanstufen im Rahmen des Vorentwurfs von Triebwerken
Effect of Incoming Boundary Layer Thickness on the Flow Characteristics of a Supersonic Air Intake
A Geometrical-Irregular Boundary Layer Suction Method for Hypersonic Flow Distortion Suppression
Advanced Parametric Lobe Mixer Concepts for Internally Mixed Nozzles
Design and Investigation of Busemann Intakes for High-Speed Propulsion Systems
Design Optimization of a Novel Boundary Layer Diverter for Semi-Submerged Inlets
Supersonic External-Compression Inlets for Mach 1.4 to 2.0
Characterization of Unsteady Distortion Events for S-Duct Intakes Under Non-Uniform Inlet Conditions
Heat Transfer Augmentation with Pin Fins in the Entry Region of Circular Channels
Comparison of Engine Models of UHBPR Turbofan at High Incidence