This thesis investigates the aerodynamic behavior of a transonic propeller operating in free flow and under Boundary Layer Ingestion (BLI) conditions. Through three-dimensional CFD , the interaction between the propeller and a non-uniform boundary layer were analyzed. The study aims to assess the influence of these operating conditions on aerodynamic performance and load distribution, offering a framework for future advancements in the design of high-efficiency propulsion systems.

This thesis investigates the aerodynamic behavior of a transonic propeller operating in free flow and under Boundary Layer Ingestion (BLI) conditions. Through three-dimensional CFD , the interaction between the propeller and a non-uniform boundary layer were analyzed. The study aims to assess the influence of these operating conditions on aerodynamic performance and load distribution, offering a framework for future advancements in the design of high-efficiency propulsion systems.

Numerical investigation of high speed propeller under boundary layer ingestion conditions

MARCHESANI, SIMONE
2024/2025

Abstract

This thesis investigates the aerodynamic behavior of a transonic propeller operating in free flow and under Boundary Layer Ingestion (BLI) conditions. Through three-dimensional CFD , the interaction between the propeller and a non-uniform boundary layer were analyzed. The study aims to assess the influence of these operating conditions on aerodynamic performance and load distribution, offering a framework for future advancements in the design of high-efficiency propulsion systems.
2024
Numerical investigation of high speed propeller under boundary layer ingestion conditions
This thesis investigates the aerodynamic behavior of a transonic propeller operating in free flow and under Boundary Layer Ingestion (BLI) conditions. Through three-dimensional CFD , the interaction between the propeller and a non-uniform boundary layer were analyzed. The study aims to assess the influence of these operating conditions on aerodynamic performance and load distribution, offering a framework for future advancements in the design of high-efficiency propulsion systems.
CFD
Propeller
NASA SR2
BLI
File in questo prodotto:
File Dimensione Formato  
Marchesani_Simone.pdf

accesso aperto

Dimensione 13.02 MB
Formato Adobe PDF
13.02 MB Adobe PDF Visualizza/Apri

The text of this website © Università degli studi di Padova. Full Text are published under a non-exclusive license. Metadata are under a CC0 License

Utilizza questo identificativo per citare o creare un link a questo documento: https://hdl.handle.net/20.500.12608/84467