Aerodynamic design of low-speed axial-flow fans: a historical overview

S Castegnaro - Designs, 2018 - mdpi.com
The paper presents a historical overview of the developments of aerodynamic design
methods for low-speed axial-flow fans. This historical overview starts from the first fan …

Free and non-free vortex design for axial fans with circumferential sweep through CFD techniques

A Angulo, RG Ramirez Gustavo… - Journal of Applied …, 2022 - jafmonline.net
The sound generated by axial flow fans has become increasingly important in several
industrial areas. These devices represent considerable noise sources that must be …

[PDF][PDF] Design and testing of an ISO 5801 inlet chamber test rig and related issues with the Standard

S Castegnaro, M Masi, A Lazzaretto - FAN 2018-International …, 2018 - researchgate.net
SUMMARY A rig has been designed and constructed according to the ISO 5801 Standard,
to test fans with a maximum inlet diameter equal to 0.8 m. The rig design procedure, that …

A New Practical Approach to the Design of Industrial Axial Fans: Tube-Axial Fans With Very Low Hub-to-Tip Ratio

M Masi, A Lazzaretto - Journal of Engineering for …, 2019 - asmedigitalcollection.asme.org
This paper presents a simple but complete design method to obtain arbitrary vortex design
tube-axial fans starting from fixed size and rotational speed. The method couples the …

A Review on Design and Optimisation of Axial Fan

V Singh, NA Baraiya - Recent Advances in Fluid Dynamics: Select …, 2022 - Springer
This paper tries to link the research that has been conducted in the field of design and
optimisation of axial fans. The attempts are made towards blade design, effects of sweep, tip …

A New Practical Approach to the Design of Industrial Axial Fans: Part II—Forward-Swept Blades With Low Hub-to-Tip Ratio

M Masi, A Lazzaretto - … Power for Land, Sea, and Air, 2019 - asmedigitalcollection.asme.org
The authors previously suggested a simple method to design forward-swept axial-flow rotors
with blades having low hub-to-tip and high aspect ratios. This design method was …

[PDF][PDF] 날개의스윕과레이크각의변화에따른튜브축류홴의공력성능평가

김장권, 오석형 - 동력시스템공학회지, 2023 - kspse.org
이번 연구에서는 날개 스팬 길이의 전압력비 가정에 의해 설계된 3 차원 튜브 축류홴의
모델을스윕과 레이크각을 변화시켜 비압축성 상태에서 대규모 와 모사로 해석하였다. 그 결과 …

Характеристики решітчастого дворядного робочого колеса вентилятора двоконтурного турбореактивного двигуна

АВ Балалаєв - 2021 - dspace.nau.edu.ua
Дисертаційну роботу присвячено вирішенню науково-прикладної задачі підвищення
ефективності дворядних лопаткових вінців вентиляторів двоконтурних …

[HTML][HTML] 날개의스윕과레이크각의변화에따른튜브축류홴의설계운전점에서하류난류유동장특성비교

김장권 - Journal of Power System Engineering-Vol, 2024 - kspse.org
초록 이번 연구는 3 차원 튜브 축류홴을 스윕과 레이크 각도를 4 가지로 변화시켜 그 유동을
비압축성 상태에서 대규모 와 모사로 해석하였다. 그 결과 설계 운전점에서 나타난 하류 …

INFLUENCE EVALUATION OF THE BLADE ANGLE OF SWEEP ON THE AERODYNAMIC LOADING OF AN AXIAL FAN OF A TURBOFAN ENGINE

АВ Балалаєв, КВ Дорошенко… - Deutsche Internationale …, 2020 - elibrary.ru
The paper presents an assessment of the influence of the sweep angle of the blades on the
aerodynamic loading of the fan impeller of a turbofan engine with a high by-pass ratio. The …