Identification and verification of the universal modeling method mathematical model
This paper presents identification and verification of a new version of the mathematical model of the Universal Modeling Method for calculating gas-dynamic characteristics of centrifugal compressors. To identify the loss model, we have tested the 20CE family of model stages designed by the Problem L...
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creator | Galerkin, Yu. B. Drozdov, A. A. Rekstin, A. F. Solovyeva, O. A. Marenina, L. N. |
description | This paper presents identification and verification of a new version of the mathematical model of the Universal Modeling Method for calculating gas-dynamic characteristics of centrifugal compressors. To identify the loss model, we have tested the 20CE family of model stages designed by the Problem Laboratory of Compressor Engineering TU Saint-Petersburg, Russia. The identification involved the results of 70 model stages tests and the plant test results of the TKR-175E and TKR-140E turbocharger compressors. The identification result was the average error in calculating the efficiency inside 1.2% for all flow rates. To verify the new model, low flow rate model stages measured characteristic were successfully compared with calculations. |
doi_str_mv | 10.1063/5.0140618 |
format | Conference Proceeding |
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B. ; Drozdov, A. A. ; Rekstin, A. F. ; Solovyeva, O. A. ; Marenina, L. N.</creator><contributor>Myshlyavtsev, Alexander V. ; Bukhtiyarov, Valerii ; Fedorova, Maria ; Fefelov, Vasiliy</contributor><creatorcontrib>Galerkin, Yu. B. ; Drozdov, A. A. ; Rekstin, A. F. ; Solovyeva, O. A. ; Marenina, L. N. ; Myshlyavtsev, Alexander V. ; Bukhtiyarov, Valerii ; Fedorova, Maria ; Fefelov, Vasiliy</creatorcontrib><description>This paper presents identification and verification of a new version of the mathematical model of the Universal Modeling Method for calculating gas-dynamic characteristics of centrifugal compressors. To identify the loss model, we have tested the 20CE family of model stages designed by the Problem Laboratory of Compressor Engineering TU Saint-Petersburg, Russia. The identification involved the results of 70 model stages tests and the plant test results of the TKR-175E and TKR-140E turbocharger compressors. The identification result was the average error in calculating the efficiency inside 1.2% for all flow rates. To verify the new model, low flow rate model stages measured characteristic were successfully compared with calculations.</description><identifier>ISSN: 0094-243X</identifier><identifier>EISSN: 1551-7616</identifier><identifier>DOI: 10.1063/5.0140618</identifier><identifier>CODEN: APCPCS</identifier><language>eng</language><publisher>Melville: American Institute of Physics</publisher><subject>Centrifugal compressors ; Dynamic characteristics ; Flow velocity ; Low flow ; Mathematical analysis ; Mathematical models ; Model testing ; Verification</subject><ispartof>AIP Conference Proceedings, 2023, Vol.2784 (1)</ispartof><rights>Author(s)</rights><rights>2023 Author(s). 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N.</creatorcontrib><title>Identification and verification of the universal modeling method mathematical model</title><title>AIP Conference Proceedings</title><description>This paper presents identification and verification of a new version of the mathematical model of the Universal Modeling Method for calculating gas-dynamic characteristics of centrifugal compressors. To identify the loss model, we have tested the 20CE family of model stages designed by the Problem Laboratory of Compressor Engineering TU Saint-Petersburg, Russia. The identification involved the results of 70 model stages tests and the plant test results of the TKR-175E and TKR-140E turbocharger compressors. The identification result was the average error in calculating the efficiency inside 1.2% for all flow rates. To verify the new model, low flow rate model stages measured characteristic were successfully compared with calculations.</description><subject>Centrifugal compressors</subject><subject>Dynamic characteristics</subject><subject>Flow velocity</subject><subject>Low flow</subject><subject>Mathematical analysis</subject><subject>Mathematical models</subject><subject>Model testing</subject><subject>Verification</subject><issn>0094-243X</issn><issn>1551-7616</issn><fulltext>true</fulltext><rsrctype>conference_proceeding</rsrctype><creationdate>2023</creationdate><recordtype>conference_proceeding</recordtype><recordid>eNpFUE1LxDAQDaLgunrwHwS8CV1nkjZNj7LourDgwT14C20ycbP0y34I_nurW_AyA--9mcd7jN0irBCUfEhWgDEo1GdsgUmCUapQnbMFQBZHIpbvl-yq748AIktTvWBvW0f1EHyw-RCamue141_U_QON58OB-FiHCe7zkleNozLUH7yi4dA4XuUTP43pYCav2YXPy55u5r1k--en_fol2r1utuvHXdRmSkZZKnRKaWE9gs2SQopEkpUgbUZEqEkBOqe9BS-8d6jRFRg7WSjyWuhCLtnd6W3bNZ8j9YM5NmNXT45G6FgIEFLApLo_qXobhr9Ipu1ClXffBsH8dmYSM3cmfwAa118-</recordid><startdate>20230726</startdate><enddate>20230726</enddate><creator>Galerkin, Yu. 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N.</creatorcontrib><collection>Technology Research Database</collection><collection>Aerospace Database</collection><collection>Advanced Technologies Database with Aerospace</collection></facets><delivery><delcategory>Remote Search Resource</delcategory><fulltext>fulltext</fulltext></delivery><addata><au>Galerkin, Yu. B.</au><au>Drozdov, A. A.</au><au>Rekstin, A. F.</au><au>Solovyeva, O. A.</au><au>Marenina, L. N.</au><au>Myshlyavtsev, Alexander V.</au><au>Bukhtiyarov, Valerii</au><au>Fedorova, Maria</au><au>Fefelov, Vasiliy</au><format>book</format><genre>proceeding</genre><ristype>CONF</ristype><atitle>Identification and verification of the universal modeling method mathematical model</atitle><btitle>AIP Conference Proceedings</btitle><date>2023-07-26</date><risdate>2023</risdate><volume>2784</volume><issue>1</issue><issn>0094-243X</issn><eissn>1551-7616</eissn><coden>APCPCS</coden><abstract>This paper presents identification and verification of a new version of the mathematical model of the Universal Modeling Method for calculating gas-dynamic characteristics of centrifugal compressors. To identify the loss model, we have tested the 20CE family of model stages designed by the Problem Laboratory of Compressor Engineering TU Saint-Petersburg, Russia. The identification involved the results of 70 model stages tests and the plant test results of the TKR-175E and TKR-140E turbocharger compressors. The identification result was the average error in calculating the efficiency inside 1.2% for all flow rates. To verify the new model, low flow rate model stages measured characteristic were successfully compared with calculations.</abstract><cop>Melville</cop><pub>American Institute of Physics</pub><doi>10.1063/5.0140618</doi><tpages>17</tpages></addata></record> |
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subjects | Centrifugal compressors Dynamic characteristics Flow velocity Low flow Mathematical analysis Mathematical models Model testing Verification |
title | Identification and verification of the universal modeling method mathematical model |
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