Evaluation of the Stress State of a Box Shell Made from Material with Different Tensile and Compressive Properties
The reduced elastic constant, the displacement of the neutral line, moments and stresses are determined for a freely supported beam made of the material with the carbon fiber frame, taking into account Hooke’s law, the hypothesis of flat cross-sections, and the equation of equilibrium of forces. The...
Gespeichert in:
| Veröffentlicht in: | Russian aeronautics 2019-04, Vol.62 (2), p.337-341 |
|---|---|
| Hauptverfasser: | , , |
| Format: | Artikel |
| Sprache: | eng |
| Schlagworte: | |
| Online-Zugang: | Volltext |
| Tags: |
Tag hinzufügen
Keine Tags, Fügen Sie den ersten Tag hinzu!
|
| container_end_page | 341 |
|---|---|
| container_issue | 2 |
| container_start_page | 337 |
| container_title | Russian aeronautics |
| container_volume | 62 |
| creator | Demidov, A. S. Kashelkin, V. V. Kapustin, E. A. |
| description | The reduced elastic constant, the displacement of the neutral line, moments and stresses are determined for a freely supported beam made of the material with the carbon fiber frame, taking into account Hooke’s law, the hypothesis of flat cross-sections, and the equation of equilibrium of forces. The proposed approach was also implemented to calculate the element of the box-section shell, which is the part of the structure of the ramjet engine for high-speed aircraft. Numerical examples are given. |
| doi_str_mv | 10.3103/S1068799819020235 |
| format | Article |
| fullrecord | <record><control><sourceid>proquest_cross</sourceid><recordid>TN_cdi_proquest_journals_2287518477</recordid><sourceformat>XML</sourceformat><sourcesystem>PC</sourcesystem><sourcerecordid>2287518477</sourcerecordid><originalsourceid>FETCH-LOGICAL-c2315-b3f08f5d9ed5a9df9be1bba347045df0d4b2ec568c9aa31d5eed740be0cde0813</originalsourceid><addsrcrecordid>eNp1UMtKAzEUDaJgrX6Au4Dr0TwmnclSa31ARaF1PWQmNzZlOhmTtOrfm6GCC3F1Dvc8LhyEzim55JTwqwUlk7KQsqSSMMK4OEAjKnmeFZLQw8STnA36MToJYU2ImLCcjZCf7VS7VdG6DjuD4wrwInoIIYGKMNwUvnGfeLGCtsVPSgM23m0Si-CtavGHjSt8a40BD13ES-iCbQGrTuOp2_RDl90BfvGuBx8thFN0ZFQb4OwHx-j1bracPmTz5_vH6fU8axinIqu5IaURWoIWSmoja6B1rXhekFxoQ3ReM2jEpGykUpxqAaCLnNRAGg2kpHyMLva9vXfvWwixWrut79LLirGyELTMiyK56N7VeBeCB1P13m6U_6ooqYZpqz_TpgzbZ0Lydm_gf5v_D30DHxd8PA</addsrcrecordid><sourcetype>Aggregation Database</sourcetype><iscdi>true</iscdi><recordtype>article</recordtype><pqid>2287518477</pqid></control><display><type>article</type><title>Evaluation of the Stress State of a Box Shell Made from Material with Different Tensile and Compressive Properties</title><source>Springer Nature - Complete Springer Journals</source><creator>Demidov, A. S. ; Kashelkin, V. V. ; Kapustin, E. A.</creator><creatorcontrib>Demidov, A. S. ; Kashelkin, V. V. ; Kapustin, E. A.</creatorcontrib><description>The reduced elastic constant, the displacement of the neutral line, moments and stresses are determined for a freely supported beam made of the material with the carbon fiber frame, taking into account Hooke’s law, the hypothesis of flat cross-sections, and the equation of equilibrium of forces. The proposed approach was also implemented to calculate the element of the box-section shell, which is the part of the structure of the ramjet engine for high-speed aircraft. Numerical examples are given.</description><identifier>ISSN: 1068-7998</identifier><identifier>EISSN: 1934-7901</identifier><identifier>DOI: 10.3103/S1068799819020235</identifier><language>eng</language><publisher>Moscow: Pleiades Publishing</publisher><subject>Automotive Engineering ; Carbon fibers ; Compressive properties ; Elastic properties ; Engineering ; Ramjet engines ; Structural Mechanics and Strength of Flight Vehicles</subject><ispartof>Russian aeronautics, 2019-04, Vol.62 (2), p.337-341</ispartof><rights>Allerton Press, Inc. 2019</rights><rights>Copyright Springer Nature B.V. 2019</rights><lds50>peer_reviewed</lds50><woscitedreferencessubscribed>false</woscitedreferencessubscribed><citedby>FETCH-LOGICAL-c2315-b3f08f5d9ed5a9df9be1bba347045df0d4b2ec568c9aa31d5eed740be0cde0813</citedby></display><links><openurl>$$Topenurl_article</openurl><openurlfulltext>$$Topenurlfull_article</openurlfulltext><thumbnail>$$Tsyndetics_thumb_exl</thumbnail><linktopdf>$$Uhttps://link.springer.com/content/pdf/10.3103/S1068799819020235$$EPDF$$P50$$Gspringer$$H</linktopdf><linktohtml>$$Uhttps://link.springer.com/10.3103/S1068799819020235$$EHTML$$P50$$Gspringer$$H</linktohtml><link.rule.ids>314,776,780,27901,27902,41464,42533,51294</link.rule.ids></links><search><creatorcontrib>Demidov, A. S.</creatorcontrib><creatorcontrib>Kashelkin, V. V.</creatorcontrib><creatorcontrib>Kapustin, E. A.</creatorcontrib><title>Evaluation of the Stress State of a Box Shell Made from Material with Different Tensile and Compressive Properties</title><title>Russian aeronautics</title><addtitle>Russ. Aeronaut</addtitle><description>The reduced elastic constant, the displacement of the neutral line, moments and stresses are determined for a freely supported beam made of the material with the carbon fiber frame, taking into account Hooke’s law, the hypothesis of flat cross-sections, and the equation of equilibrium of forces. The proposed approach was also implemented to calculate the element of the box-section shell, which is the part of the structure of the ramjet engine for high-speed aircraft. Numerical examples are given.</description><subject>Automotive Engineering</subject><subject>Carbon fibers</subject><subject>Compressive properties</subject><subject>Elastic properties</subject><subject>Engineering</subject><subject>Ramjet engines</subject><subject>Structural Mechanics and Strength of Flight Vehicles</subject><issn>1068-7998</issn><issn>1934-7901</issn><fulltext>true</fulltext><rsrctype>article</rsrctype><creationdate>2019</creationdate><recordtype>article</recordtype><recordid>eNp1UMtKAzEUDaJgrX6Au4Dr0TwmnclSa31ARaF1PWQmNzZlOhmTtOrfm6GCC3F1Dvc8LhyEzim55JTwqwUlk7KQsqSSMMK4OEAjKnmeFZLQw8STnA36MToJYU2ImLCcjZCf7VS7VdG6DjuD4wrwInoIIYGKMNwUvnGfeLGCtsVPSgM23m0Si-CtavGHjSt8a40BD13ES-iCbQGrTuOp2_RDl90BfvGuBx8thFN0ZFQb4OwHx-j1bracPmTz5_vH6fU8axinIqu5IaURWoIWSmoja6B1rXhekFxoQ3ReM2jEpGykUpxqAaCLnNRAGg2kpHyMLva9vXfvWwixWrut79LLirGyELTMiyK56N7VeBeCB1P13m6U_6ooqYZpqz_TpgzbZ0Lydm_gf5v_D30DHxd8PA</recordid><startdate>20190401</startdate><enddate>20190401</enddate><creator>Demidov, A. S.</creator><creator>Kashelkin, V. V.</creator><creator>Kapustin, E. A.</creator><general>Pleiades Publishing</general><general>Springer Nature B.V</general><scope>AAYXX</scope><scope>CITATION</scope><scope>8FD</scope><scope>H8D</scope><scope>L7M</scope></search><sort><creationdate>20190401</creationdate><title>Evaluation of the Stress State of a Box Shell Made from Material with Different Tensile and Compressive Properties</title><author>Demidov, A. S. ; Kashelkin, V. V. ; Kapustin, E. A.</author></sort><facets><frbrtype>5</frbrtype><frbrgroupid>cdi_FETCH-LOGICAL-c2315-b3f08f5d9ed5a9df9be1bba347045df0d4b2ec568c9aa31d5eed740be0cde0813</frbrgroupid><rsrctype>articles</rsrctype><prefilter>articles</prefilter><language>eng</language><creationdate>2019</creationdate><topic>Automotive Engineering</topic><topic>Carbon fibers</topic><topic>Compressive properties</topic><topic>Elastic properties</topic><topic>Engineering</topic><topic>Ramjet engines</topic><topic>Structural Mechanics and Strength of Flight Vehicles</topic><toplevel>peer_reviewed</toplevel><toplevel>online_resources</toplevel><creatorcontrib>Demidov, A. S.</creatorcontrib><creatorcontrib>Kashelkin, V. V.</creatorcontrib><creatorcontrib>Kapustin, E. A.</creatorcontrib><collection>CrossRef</collection><collection>Technology Research Database</collection><collection>Aerospace Database</collection><collection>Advanced Technologies Database with Aerospace</collection><jtitle>Russian aeronautics</jtitle></facets><delivery><delcategory>Remote Search Resource</delcategory><fulltext>fulltext</fulltext></delivery><addata><au>Demidov, A. S.</au><au>Kashelkin, V. V.</au><au>Kapustin, E. A.</au><format>journal</format><genre>article</genre><ristype>JOUR</ristype><atitle>Evaluation of the Stress State of a Box Shell Made from Material with Different Tensile and Compressive Properties</atitle><jtitle>Russian aeronautics</jtitle><stitle>Russ. Aeronaut</stitle><date>2019-04-01</date><risdate>2019</risdate><volume>62</volume><issue>2</issue><spage>337</spage><epage>341</epage><pages>337-341</pages><issn>1068-7998</issn><eissn>1934-7901</eissn><abstract>The reduced elastic constant, the displacement of the neutral line, moments and stresses are determined for a freely supported beam made of the material with the carbon fiber frame, taking into account Hooke’s law, the hypothesis of flat cross-sections, and the equation of equilibrium of forces. The proposed approach was also implemented to calculate the element of the box-section shell, which is the part of the structure of the ramjet engine for high-speed aircraft. Numerical examples are given.</abstract><cop>Moscow</cop><pub>Pleiades Publishing</pub><doi>10.3103/S1068799819020235</doi><tpages>5</tpages></addata></record> |
| fulltext | fulltext |
| identifier | ISSN: 1068-7998 |
| ispartof | Russian aeronautics, 2019-04, Vol.62 (2), p.337-341 |
| issn | 1068-7998 1934-7901 |
| language | eng |
| recordid | cdi_proquest_journals_2287518477 |
| source | Springer Nature - Complete Springer Journals |
| subjects | Automotive Engineering Carbon fibers Compressive properties Elastic properties Engineering Ramjet engines Structural Mechanics and Strength of Flight Vehicles |
| title | Evaluation of the Stress State of a Box Shell Made from Material with Different Tensile and Compressive Properties |
| url | https://sfx.bib-bvb.de/sfx_tum?ctx_ver=Z39.88-2004&ctx_enc=info:ofi/enc:UTF-8&ctx_tim=2025-02-01T12%3A22%3A10IST&url_ver=Z39.88-2004&url_ctx_fmt=infofi/fmt:kev:mtx:ctx&rfr_id=info:sid/primo.exlibrisgroup.com:primo3-Article-proquest_cross&rft_val_fmt=info:ofi/fmt:kev:mtx:journal&rft.genre=article&rft.atitle=Evaluation%20of%20the%20Stress%20State%20of%20a%20Box%20Shell%20Made%20from%20Material%20with%20Different%20Tensile%20and%20Compressive%20Properties&rft.jtitle=Russian%20aeronautics&rft.au=Demidov,%20A.%20S.&rft.date=2019-04-01&rft.volume=62&rft.issue=2&rft.spage=337&rft.epage=341&rft.pages=337-341&rft.issn=1068-7998&rft.eissn=1934-7901&rft_id=info:doi/10.3103/S1068799819020235&rft_dat=%3Cproquest_cross%3E2287518477%3C/proquest_cross%3E%3Curl%3E%3C/url%3E&disable_directlink=true&sfx.directlink=off&sfx.report_link=0&rft_id=info:oai/&rft_pqid=2287518477&rft_id=info:pmid/&rfr_iscdi=true |