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
CFD Modeling of Turbofan Intake Aerodynamics at Crosswind Conditions
Effect of Small Step on Aerodynamic Performance in the Transonic Inlet
Design Optimization of a Fan Blade Under Boundary Layer Ingestion Flow
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
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
Methodology of Turbulence Model Tuning for Air Inlet CFD Simulations
Effects of Non-Uniform Inflow to Side- And Central- Spillage Bump Inlets
Data-Driven Modelling Tradeoffs to Characterize the Distortion Profile of an APU Inlet
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
Comprehensive Assessments of Hypersonic Inlet Restart Using Active Jet
Viscous Wake Effects on the Inviscid Wall-Bounded Jet Flow Over an Aerospike Nozzle
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
Brayton Cycle Analysis of the Effect of Wake Ingestion on Aircraft Range
Spectral Proper Orthogonal Decomposition Downstream of a Vortex Tube Separator Array
FUN3D Analyses of the 5th AIAA Propulsion Aerodynamics Workshop Inlet Test Case
Computational Assessment of Non-Axisymmetric Separate-Jet Exhausts on Test Rig Configurations
Design Considerations of Non-Axisymmetric Exhausts for Large Civil Aero-Engines