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Lateral Thrust Units and Manoeuvring Propulsion Devices
Numerical Study of Supersonic Jet Characteristics of Underwater Solid Rocket Engine
Computational Analysis and Regression Laws for Nozzle Erosion Prediction in Hybrid Rockets
Steady Versus Unsteady Pneumatic Flow Control and Aspects of Practical Integration
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
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
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
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
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
FUN3D Analyses of the 5th AIAA Propulsion Aerodynamics Workshop Inlet Test Case
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
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