Call For Paper Volume:7 Issue:9 Sep'2020 |

PERFORMANCE ANALYSIS OF SINGLE STAGE CENTIFUGALOMPRESSOR BY CHANGING ITS INLET BLADE ANGLE

Publication Date : 17/10/2016


DOI : 10.21884/IJMTER.2016.3088.ODIPA

Author(s) :

dhruv joshi , Dhruv Joshi , Nawaz Qureshi , Jigar V. Bhalodiya.


Volume/Issue :
Volume 3
,
Issue 10
(10 - 2016)



Abstract :

This Project shows the change in Performance of the Centrifugal Compressor by changing its inlet blade angle with medium pressure ratio centrifugal Compressor. Compute of parameter which got influenced by change of inlet blade angle. Determine the performance of centrifugal compressor by change of its blade angle. The design code provides a basis on which the design of the Compressor can be modeled by varying the key parameters which include both aerodynamic and geometric details. Code than will predict first cut solution. The design which models the flow in an Impeller, and an annular bend takes into consideration various loss models occurring in the complex flow of a Centrifugal Compressor. Whole compressor is modeled & Assemble in Creo 3.0 and validated in ANSYS14.5.


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PERFORMANCE ANALYSIS OF SINGLE STAGE CENTIFUGALOMPRESSOR BY CHANGING ITS INLET BLADE ANGLE

September 14, 2016