Stall inception mechanisms in a contra-rotating fan operating at different speed combinations
Contra-rotating fan is a concept that can possibly replace the present-day conventional fans due to its several aerodynamic advantages. It has the potential to improve the stability limit and can achieve a higher pressure ratio per stage. One of the advantages of a contra-rotating fan is its capabil...
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Veröffentlicht in: | Proceedings of the Institution of Mechanical Engineers. Part A, Journal of power and energy Journal of power and energy, 2020-12, Vol.234 (8), p.1041-1052 |
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description | Contra-rotating fan is a concept that can possibly replace the present-day conventional fans due to its several aerodynamic advantages. It has the potential to improve the stability limit and can achieve a higher pressure ratio per stage. One of the advantages of a contra-rotating fan is its capability to operate both the rotors at different speeds. In the present study, experiments are carried out at different speed combinations of the rotors and the stall inception phenomenon is captured using high-response unsteady pressure sensors placed on the casing upstream of the leading edge of rotor-1. The unsteady pressure data are investigated using wavelet and Fourier analysis techniques. It is observed that the mechanism of stall inception is different for different speed combinations. The pre-stall disturbances fall in different frequency ranges for different speed combinations. For the range of speed combinations investigated, the frequency of appearance of stall cells of rotor-1 does not depend on the speed of rotor-2. A higher speed of rotation of rotor-1 leads to a higher frequency of appearance of stall cells and a lower speed of rotation of rotor-1 leads to a lower frequency of appearance of stall cells. For all the speed combinations, there is a range of frequency where no disturbance is observed and this range is termed as the ‘no-disturbance zone’. Disturbances are observed at lower frequencies and at frequencies close to the blade passing frequency. In order to understand the flow physics in detail, computational analysis is carried out for different speed combinations of the rotors. For a higher speed of rotor-2, it is observed that the suction effect of rotor-2 is significant enough to pull the tip-leakage flow towards the axial direction. Thus, the suction effect of rotor-2 plays a significant role in determining the stall of the stage. |
doi_str_mv | 10.1177/0957650919893831 |
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It has the potential to improve the stability limit and can achieve a higher pressure ratio per stage. One of the advantages of a contra-rotating fan is its capability to operate both the rotors at different speeds. In the present study, experiments are carried out at different speed combinations of the rotors and the stall inception phenomenon is captured using high-response unsteady pressure sensors placed on the casing upstream of the leading edge of rotor-1. The unsteady pressure data are investigated using wavelet and Fourier analysis techniques. It is observed that the mechanism of stall inception is different for different speed combinations. The pre-stall disturbances fall in different frequency ranges for different speed combinations. For the range of speed combinations investigated, the frequency of appearance of stall cells of rotor-1 does not depend on the speed of rotor-2. A higher speed of rotation of rotor-1 leads to a higher frequency of appearance of stall cells and a lower speed of rotation of rotor-1 leads to a lower frequency of appearance of stall cells. For all the speed combinations, there is a range of frequency where no disturbance is observed and this range is termed as the ‘no-disturbance zone’. Disturbances are observed at lower frequencies and at frequencies close to the blade passing frequency. In order to understand the flow physics in detail, computational analysis is carried out for different speed combinations of the rotors. For a higher speed of rotor-2, it is observed that the suction effect of rotor-2 is significant enough to pull the tip-leakage flow towards the axial direction. Thus, the suction effect of rotor-2 plays a significant role in determining the stall of the stage.</description><identifier>ISSN: 0957-6509</identifier><identifier>EISSN: 2041-2967</identifier><identifier>DOI: 10.1177/0957650919893831</identifier><language>eng</language><publisher>London, England: SAGE Publications</publisher><subject>Aerodynamic stability ; Disturbances ; Fourier analysis ; Frequency ranges ; Pressure ratio ; Pressure sensors ; Rotation ; Rotors ; Stalling ; Suction ; Wavelet analysis</subject><ispartof>Proceedings of the Institution of Mechanical Engineers. 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Part A, Journal of power and energy</title><description>Contra-rotating fan is a concept that can possibly replace the present-day conventional fans due to its several aerodynamic advantages. It has the potential to improve the stability limit and can achieve a higher pressure ratio per stage. One of the advantages of a contra-rotating fan is its capability to operate both the rotors at different speeds. In the present study, experiments are carried out at different speed combinations of the rotors and the stall inception phenomenon is captured using high-response unsteady pressure sensors placed on the casing upstream of the leading edge of rotor-1. The unsteady pressure data are investigated using wavelet and Fourier analysis techniques. It is observed that the mechanism of stall inception is different for different speed combinations. The pre-stall disturbances fall in different frequency ranges for different speed combinations. For the range of speed combinations investigated, the frequency of appearance of stall cells of rotor-1 does not depend on the speed of rotor-2. A higher speed of rotation of rotor-1 leads to a higher frequency of appearance of stall cells and a lower speed of rotation of rotor-1 leads to a lower frequency of appearance of stall cells. For all the speed combinations, there is a range of frequency where no disturbance is observed and this range is termed as the ‘no-disturbance zone’. Disturbances are observed at lower frequencies and at frequencies close to the blade passing frequency. In order to understand the flow physics in detail, computational analysis is carried out for different speed combinations of the rotors. For a higher speed of rotor-2, it is observed that the suction effect of rotor-2 is significant enough to pull the tip-leakage flow towards the axial direction. Thus, the suction effect of rotor-2 plays a significant role in determining the stall of the stage.</description><subject>Aerodynamic stability</subject><subject>Disturbances</subject><subject>Fourier analysis</subject><subject>Frequency ranges</subject><subject>Pressure ratio</subject><subject>Pressure sensors</subject><subject>Rotation</subject><subject>Rotors</subject><subject>Stalling</subject><subject>Suction</subject><subject>Wavelet analysis</subject><issn>0957-6509</issn><issn>2041-2967</issn><fulltext>true</fulltext><rsrctype>article</rsrctype><creationdate>2020</creationdate><recordtype>article</recordtype><recordid>eNp1UEtLxDAQDqLgunr3GPBczaNpmqMsvmDBg3qUMkkna5dtWpPswX9vlwqC4FyGme8FHyGXnF1zrvUNM0pXihluaiNryY_IQrCSF8JU-pgsDnBxwE_JWUpbNo3SYkHeXzLsdrQLDsfcDYH26D4gdKlP05MCdUPIEYo4ZMhd2FAPgQ4jxvmCTNvOe4wYMk0jYjsJetsFOJilc3LiYZfw4mcvydv93evqsVg_PzytbteFk8zkAmqAGq0QTtaKgbfcSw9oJXdeK82Vq5zwXpfMllXrVYlWG6Mk6raqLLdySa5m3zEOn3tMudkO-ximyEaUUimmlOATi80sF4eUIvpmjF0P8avhrDmU2PwtcZIUsyTBBn9N_-V_A7NVcuc</recordid><startdate>202012</startdate><enddate>202012</enddate><creator>Manas, MP</creator><creator>Pradeep, AM</creator><general>SAGE Publications</general><general>SAGE PUBLICATIONS, INC</general><scope>AAYXX</scope><scope>CITATION</scope><scope>7SP</scope><scope>7TB</scope><scope>8FD</scope><scope>F28</scope><scope>FR3</scope><scope>KR7</scope><scope>L7M</scope><orcidid>https://orcid.org/0000-0002-8893-7548</orcidid><orcidid>https://orcid.org/0000-0001-5218-9106</orcidid></search><sort><creationdate>202012</creationdate><title>Stall inception mechanisms in a contra-rotating fan operating at different speed combinations</title><author>Manas, MP ; Pradeep, AM</author></sort><facets><frbrtype>5</frbrtype><frbrgroupid>cdi_FETCH-LOGICAL-c309t-a8aa8eb22c3850afb1f3faeb31cf75715c6c2ff740b46df54eb79953e7d66b1b3</frbrgroupid><rsrctype>articles</rsrctype><prefilter>articles</prefilter><language>eng</language><creationdate>2020</creationdate><topic>Aerodynamic stability</topic><topic>Disturbances</topic><topic>Fourier analysis</topic><topic>Frequency ranges</topic><topic>Pressure ratio</topic><topic>Pressure sensors</topic><topic>Rotation</topic><topic>Rotors</topic><topic>Stalling</topic><topic>Suction</topic><topic>Wavelet analysis</topic><toplevel>peer_reviewed</toplevel><toplevel>online_resources</toplevel><creatorcontrib>Manas, MP</creatorcontrib><creatorcontrib>Pradeep, AM</creatorcontrib><collection>CrossRef</collection><collection>Electronics & Communications Abstracts</collection><collection>Mechanical & Transportation Engineering Abstracts</collection><collection>Technology Research Database</collection><collection>ANTE: Abstracts in New Technology & Engineering</collection><collection>Engineering Research Database</collection><collection>Civil Engineering Abstracts</collection><collection>Advanced Technologies Database with Aerospace</collection><jtitle>Proceedings of the Institution of Mechanical Engineers. Part A, Journal of power and energy</jtitle></facets><delivery><delcategory>Remote Search Resource</delcategory><fulltext>fulltext</fulltext></delivery><addata><au>Manas, MP</au><au>Pradeep, AM</au><format>journal</format><genre>article</genre><ristype>JOUR</ristype><atitle>Stall inception mechanisms in a contra-rotating fan operating at different speed combinations</atitle><jtitle>Proceedings of the Institution of Mechanical Engineers. Part A, Journal of power and energy</jtitle><date>2020-12</date><risdate>2020</risdate><volume>234</volume><issue>8</issue><spage>1041</spage><epage>1052</epage><pages>1041-1052</pages><issn>0957-6509</issn><eissn>2041-2967</eissn><abstract>Contra-rotating fan is a concept that can possibly replace the present-day conventional fans due to its several aerodynamic advantages. It has the potential to improve the stability limit and can achieve a higher pressure ratio per stage. One of the advantages of a contra-rotating fan is its capability to operate both the rotors at different speeds. In the present study, experiments are carried out at different speed combinations of the rotors and the stall inception phenomenon is captured using high-response unsteady pressure sensors placed on the casing upstream of the leading edge of rotor-1. The unsteady pressure data are investigated using wavelet and Fourier analysis techniques. It is observed that the mechanism of stall inception is different for different speed combinations. The pre-stall disturbances fall in different frequency ranges for different speed combinations. For the range of speed combinations investigated, the frequency of appearance of stall cells of rotor-1 does not depend on the speed of rotor-2. A higher speed of rotation of rotor-1 leads to a higher frequency of appearance of stall cells and a lower speed of rotation of rotor-1 leads to a lower frequency of appearance of stall cells. For all the speed combinations, there is a range of frequency where no disturbance is observed and this range is termed as the ‘no-disturbance zone’. Disturbances are observed at lower frequencies and at frequencies close to the blade passing frequency. In order to understand the flow physics in detail, computational analysis is carried out for different speed combinations of the rotors. For a higher speed of rotor-2, it is observed that the suction effect of rotor-2 is significant enough to pull the tip-leakage flow towards the axial direction. Thus, the suction effect of rotor-2 plays a significant role in determining the stall of the stage.</abstract><cop>London, England</cop><pub>SAGE Publications</pub><doi>10.1177/0957650919893831</doi><tpages>12</tpages><orcidid>https://orcid.org/0000-0002-8893-7548</orcidid><orcidid>https://orcid.org/0000-0001-5218-9106</orcidid></addata></record> |
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subjects | Aerodynamic stability Disturbances Fourier analysis Frequency ranges Pressure ratio Pressure sensors Rotation Rotors Stalling Suction Wavelet analysis |
title | Stall inception mechanisms in a contra-rotating fan operating at different speed combinations |
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