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
Angle of Attack Effects on Open Fan Propulsion Systems at Take-Off Conditions
Design and Analysis of a Jet Stretcher for High-Altitude Supersonic Free Jet Testing
Design Optimization of a Novel Boundary Layer Diverter for Semi-Submerged Inlets
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
Methodology of Turbulence Model Tuning for Air Inlet CFD Simulations
Computational Assessment of Non-Axisymmetric Separate-Jet Exhausts on Test Rig Configurations
Design Considerations of Non-Axisymmetric Exhausts for Large Civil Aero-Engines
Parametric Study on the Thrust Vectoring of a Supersonic Jet Manipulated by Fluidic Injection
Flow Separation Measurements in Regions of SBLI Using Wall Shear Sensors
Computational Study of an Internal Osculating Waverider Intake
Brayton Cycle Analysis of the Effect of Wake Ingestion on Aircraft Range
Spectral Proper Orthogonal Decomposition Downstream of a Vortex Tube Separator Array
Surface Pressure Comparison of an Internal Osculating Waverider Inlet Under Noisy and Quiet Flow
Nacelle 3D Aerodynamic Design and Airframe Integration for an Over Wing Configuration
Multiobjective Aerodynamic Design Optimization of the Contour of Annular Aerospike Nozzles
PIV Measurements of Internal Flows Through Nozzles with Curvature and Shape Transition
FUN3D Analyses of the 5th AIAA Propulsion Aerodynamics Workshop Inlet Test Case
Comprehensive Assessments of Hypersonic Inlet Restart Using Active Jet
Viscous Wake Effects on the Inviscid Wall-Bounded Jet Flow Over an Aerospike Nozzle
Deep-Learning for Flow-Field Prediction of 3D Non-Axisymmetric Aero-Engine Nacelles
Design of a High-Speed Intake Distortion Simulator for Propulsion Integration Research