Reaktivnye sopla perspektivnych graždanskich samoletov : sbornik statej
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
BCFD Analysis for the 5th AIAA Propulsion Aerodynamics Workshop: Film Cooled Nozzle Results
Design of Short Intakes for Ultra-High Bypass Engines: Preliminary Exploration at Fixed Incidence
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
Computational Assessment of Non-Axisymmetric Separate-Jet Exhausts on Test Rig Configurations
Design Considerations of Non-Axisymmetric Exhausts for Large Civil Aero-Engines
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
Methodology of Turbulence Model Tuning for Air Inlet CFD Simulations
Summary of the 5th Propulsion Aerodynamics Workshop: Inlet Cross-Flow Results
Some Design Considerations for Two-Dimensional, Mixed-Compression Inlets for Mach 2.5 to 3.5
Assessment of Engine Modelling on the Installed Aerodynamics of an Ultra-High Bypass Turbofan
Conjugate Heat-Transfer Simulations of a Rectangular Nozzle Exhaust Flow Over a Film-Cooled Plate
Comparison of CFD Ground Vortex Results with the 5th PAW Intake Near the Ground Experiment
INVESTIGATION OF HL-CRM AERODYNAMICS WITH A UHBPR NACELLE IN POWERED-ON CONDITION
SENSITIVITY ANALYSIS OF NACELLE INTAKE HIGH-INCIDENCE AERODYNAMICS INCLUDING A BODY FORCE FAN MODEL
CARTESIAN MESH SIMULATIONS FOR THE THIRD AIAA SONIC BOOM PREDICTION WORKSHOP
DLR TAU SIMULATIONS FOR THE THIRD AIAA SONIC BOOM PREDICTION WORKSHOP NEAR-FIELD CASES
INSTABILITY AND NOISE GENERATION FROM THERMALLY NON-UNIFORM SUPERSONIC JETS WITH OFFSET
NUMERICAL AND EXPERIMENTAL RESEARCH FOR AN UNCONVENTIONAL TURBOSHAFT INTAKE MANIFOLD