The inverse design is one of the aerodynamic design methods, in which the pressure
distribution along the wall is known, and the duct geometry is unknown. To obtain the best …

In this study, the unique reverse-flow around the inlet nozzle of a squirrel-cage fan was
numerically studied by computational fluid dynamics (CFD), and a non-axisymmetric D-type …

The goal of the present study is to improve aerodynamic performance of the helicopter main
rotor by geometric redesign of its blades' tips. In this process, the generated noise is …

Counter-rotating axial-flow compressor (CRAC) is a promising technology to increase the
thrust-to-weight ratio of aero-engines. Self-recirculating casing treatment (SRCT) is selected …

In a boundary layer ingestion (BLI) propulsion system, the compressor rotor operates under
the condition of a severe inflow distortion because the boundary layers on the surface of …

In this study, the blade shape of the squirrel-cage fan system inside the range hood was
optimized using the surrogate model to improve the maximum volume flow rate. The …

Trajectory planning is a complex problem, which involves meeting the physical constraints of
the Unmanned Aerial Vehicles (UAVs), constraints from the operating environment and …

Purpose This study aims to study the radar cross-section (RCS) of an intermeshing rotor with
blade pitch. Design/methodology/approach The variation of rotor blade pitch is designed …

Conventional processes require a mould for the manufacture of each test product, which
often results in high costs but is ideal for large series of products. In contrast, for prototypes …

This study explores the effects of leading-edge tubercles applied to a canonical rotor blade
in an effort to improve aerodynamic performance of a rotor in hover, without sacrificing …