Numerical sensitivity analysis of axial flow fan 3d aerodynamics under off design conditions

Praveen Kumar Akula, Balbir Singh, Vishnu G. Nair

Research output: Chapter in Book/Report/Conference proceedingConference contribution

Abstract

Compressor is a crucial component of an engine. Flow through the compressor is intricate and sensitive to the reference frame, geometry of the blade, tip clearance, stator, staging, etc. Compressor, though designed for a particular environment, is also expected to show its performance under off design conditions like accelerating flight, landing, take off, climbing etc. The flow in third dimension leads to many complications and ambiguity. Tip aerodynamics, passage flow, and vortex aerodynamics play crucial role in describing the flow through the upper half of the blade and in the tip region, whereas flow over blade surface, trailing edge and the hub will guide the aerodynamic behavior of the rotor blade. This exercise is done for off design environment to study the aforesaid flow characteristics and is carried on an axial flow fan. The performance variation of fan flow under varying flow conditions is analyzed.

Original languageEnglish
Title of host publicationAEROTECH IV - Recent Advances in Aerospace Technologies
Pages8-12
Number of pages5
Volume225
DOIs
Publication statusPublished - 2012
EventAEROTECH IV - 2012 - Kuala Lumpur, Malaysia
Duration: 21-11-201222-11-2012

Publication series

NameApplied Mechanics and Materials
Volume225
ISSN (Print)1660-9336
ISSN (Electronic)1662-7482

Conference

ConferenceAEROTECH IV - 2012
CountryMalaysia
CityKuala Lumpur
Period21-11-1222-11-12

All Science Journal Classification (ASJC) codes

  • Engineering(all)

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  • Cite this

    Akula, P. K., Singh, B., & Nair, V. G. (2012). Numerical sensitivity analysis of axial flow fan 3d aerodynamics under off design conditions. In AEROTECH IV - Recent Advances in Aerospace Technologies (Vol. 225, pp. 8-12). (Applied Mechanics and Materials; Vol. 225). https://doi.org/10.4028/www.scientific.net/AMM.225.8