Abstract: A blade leading edge spike flow can usually be found on the condition that the discontinuous curvature curves between blade leading edge and blade surface, which is a common result of design ...

ABSTRACT: This paper presents two optimized rotors. The first rotor is as part of a 3-blade row optimization (IGV-rotor-stator) of a high-pressure compressor. It is based on modifying blade angles and ...

Axial compressors are critical components in aero-engines and industrial gas turbines, where blade vibration and aerodynamics are inextricably linked to performance and safety. Current research has ...

The study of aerodynamic performance in compressor blades is critical for optimising the efficiency and reliability of modern turbomachinery. Recent work has focused on the dual challenges of ...

BEIJING, Sept. 9, 2020 /PRNewswire/ -- The super-large axial compressor unit AV140, innovatively developed by Shaanxi Blower (Group) Co., Ltd., has successfully completed its test run in the plant on ...