Response Analysis of Projectile System Under Gaussian Noise Excitation Using Path Integral Method
During flight, projectiles are subject to uncertainties such as aerodynamic forces, wind gusts, and measurement errors; all of which significantly affect their stability and accuracy. As a result, studying the response of projectile systems under stochastic excitation is essential. This paper focuse...
Saved in:
Published in | International Journal of Aerospace Engineering Vol. 2024; no. 1 |
---|---|
Main Authors | , , , , |
Format | Journal Article |
Language | English |
Published |
New York
John Wiley & Sons, Inc
02.12.2024
Wiley |
Subjects | |
Online Access | Get full text |
Cover
Loading…
Abstract | During flight, projectiles are subject to uncertainties such as aerodynamic forces, wind gusts, and measurement errors; all of which significantly affect their stability and accuracy. As a result, studying the response of projectile systems under stochastic excitation is essential. This paper focuses on the solution and analysis of projectile system responses under stochastic excitation. We employed the path integral method to compute the transient and stationary probability density functions for projectile systems subjected to Gaussian stochastic external and parametric excitations. Based on the probabilistic responses, we analyzed the evolution of the system’s probability density function over time under Gaussian white noise excitation, as well as the changes in the stationary probability density function with air density and flight speed as bifurcation parameters. The analysis results indicate that within a specific range of parameter variations, air density can induce stochastic P‐bifurcation phenomena. Furthermore, increasing air density and flight speed can enhance the stability of the projectile. |
---|---|
AbstractList | During flight, projectiles are subject to uncertainties such as aerodynamic forces, wind gusts, and measurement errors; all of which significantly affect their stability and accuracy. As a result, studying the response of projectile systems under stochastic excitation is essential. This paper focuses on the solution and analysis of projectile system responses under stochastic excitation. We employed the path integral method to compute the transient and stationary probability density functions for projectile systems subjected to Gaussian stochastic external and parametric excitations. Based on the probabilistic responses, we analyzed the evolution of the system’s probability density function over time under Gaussian white noise excitation, as well as the changes in the stationary probability density function with air density and flight speed as bifurcation parameters. The analysis results indicate that within a specific range of parameter variations, air density can induce stochastic P‐bifurcation phenomena. Furthermore, increasing air density and flight speed can enhance the stability of the projectile. |
Audience | Academic |
Author | Peng, Jiahui Dong, Shuangqi Zhang, Zhonghua Wang, Liang Li, Xinyi |
Author_xml | – sequence: 1 givenname: Liang surname: Wang fullname: Wang, Liang – sequence: 2 givenname: Xinyi orcidid: 0009-0008-2521-0350 surname: Li fullname: Li, Xinyi – sequence: 3 givenname: Jiahui orcidid: 0009-0008-1532-125X surname: Peng fullname: Peng, Jiahui – sequence: 4 givenname: Zhonghua orcidid: 0009-0000-1641-3334 surname: Zhang fullname: Zhang, Zhonghua – sequence: 5 givenname: Shuangqi orcidid: 0009-0009-0641-1752 surname: Dong fullname: Dong, Shuangqi |
BookMark | eNptklFLHDEUhQexULW-9QcEfCp0NZnJTCaPi1i7YFXUfQ53Mjdjhtlkm2TB_ffNdkW6UPJwQ_jOgZx7Totj5x0WxVdGLxmr6ys7Al4JUdKGlUfFCWtaMaul4Mcf96b5XJzGOFLa0FrUJwU8YVx7F5HMHUzbaCPxhjwGP6JOdkLyvI0JV2TpegzkFjYxWnDk3tssuXnTNkGy3pFltG4gj5BeycIlHAJM5BemV99_KT4ZmCKev8-zYvnj5uX65-zu4XZxPb-baV6KNJPMiLoTdQNt38oGRUvLtuy7CrgWRkqhGTO05EY3FCouetNxg5IL0ZWUMazOisXet_cwqnWwKwhb5cGqvw8-DApCsnpCxU2JrKEtallxbljLmYGOljIbmYpV2eti77UO_vcGY1Kj34QcUFQV41ywmst_qAGyqXXGpwB6ZaNW85ZJWVMq20xd_ofKp8eV1XmBJsd8KPh2IMhMwrc07LJXi-enQ_b7ntXBxxjQfHycUbXrhNp1Qr13ovoDGRSoRw |
Cites_doi | 10.1103/PhysRevA.35.1795 10.1016/S0020-7462(96)00096-0 10.1016/j.ijnonlinmec.2023.104504 10.2514/3.25343 10.1016/j.ymssp.2012.02.013 10.1016/j.taml.2022.100385 10.2514/3.50025 10.1016/S0266-8920(99)00031-4 10.1016/j.jsv.2023.118037 10.1007/s11071-019-05159-3 10.1007/s11071-014-1310-8 10.1103/PhysRevA.28.3003 10.1016/j.strusafe.2015.11.001 10.21236/AD0442757 10.1007/s11071-016-3323-y 10.1016/0096-3003(90)90003-L 10.1007/s00707-013-1040-x 10.1016/j.ast.2016.10.016 10.2514/1.A33864 |
ContentType | Journal Article |
Copyright | COPYRIGHT 2024 John Wiley & Sons, Inc. Copyright © 2024 Liang Wang et al. This is an open access article distributed under the Creative Commons Attribution License (the “License”), which permits unrestricted use, distribution, and reproduction in any medium, provided the original work is properly cited. Notwithstanding the ProQuest Terms and Conditions, you may use this content in accordance with the terms of the License. https://creativecommons.org/licenses/by/4.0 |
Copyright_xml | – notice: COPYRIGHT 2024 John Wiley & Sons, Inc. – notice: Copyright © 2024 Liang Wang et al. This is an open access article distributed under the Creative Commons Attribution License (the “License”), which permits unrestricted use, distribution, and reproduction in any medium, provided the original work is properly cited. Notwithstanding the ProQuest Terms and Conditions, you may use this content in accordance with the terms of the License. https://creativecommons.org/licenses/by/4.0 |
DBID | AAYXX CITATION ISR 7TB 8FD 8FE 8FG ABJCF ABUWG AFKRA ARAPS AZQEC BENPR BGLVJ CCPQU CWDGH DWQXO FR3 H8D HCIFZ L6V L7M M7S P5Z P62 PHGZM PHGZT PIMPY PKEHL PQEST PQGLB PQQKQ PQUKI PRINS PTHSS DOA |
DOI | 10.1155/ijae/7720612 |
DatabaseName | CrossRef Gale In Context: Science Mechanical & Transportation Engineering Abstracts Technology Research Database ProQuest SciTech Collection ProQuest Technology Collection SciTech Premium Collection ProQuest Central (Alumni) ProQuest Central UK/Ireland Advanced Technologies & Aerospace Collection ProQuest Central Essentials ProQuest Central Technology Collection ProQuest One Community College Middle East & Africa Database ProQuest Central Korea Engineering Research Database Aerospace Database SciTech Premium Collection ProQuest Engineering Collection Advanced Technologies Database with Aerospace Engineering Database Advanced Technologies & Aerospace Database ProQuest Advanced Technologies & Aerospace Collection ProQuest Central Premium ProQuest One Academic Publicly Available Content Database ProQuest One Academic Middle East (New) ProQuest One Academic Eastern Edition (DO NOT USE) ProQuest One Applied & Life Sciences ProQuest One Academic ProQuest One Academic UKI Edition ProQuest Central China Engineering Collection DOAJ Directory of Open Access Journals |
DatabaseTitle | CrossRef Publicly Available Content Database Technology Collection Technology Research Database ProQuest One Academic Middle East (New) Mechanical & Transportation Engineering Abstracts ProQuest Advanced Technologies & Aerospace Collection ProQuest Central Essentials ProQuest Central (Alumni Edition) SciTech Premium Collection ProQuest One Community College ProQuest Central China ProQuest Central ProQuest One Applied & Life Sciences Aerospace Database ProQuest Engineering Collection Middle East & Africa Database ProQuest Central Korea ProQuest Central (New) Advanced Technologies Database with Aerospace Engineering Collection Advanced Technologies & Aerospace Collection Engineering Database ProQuest One Academic Eastern Edition ProQuest Technology Collection ProQuest SciTech Collection Advanced Technologies & Aerospace Database ProQuest One Academic UKI Edition Materials Science & Engineering Collection Engineering Research Database ProQuest One Academic ProQuest One Academic (New) |
DatabaseTitleList | CrossRef |
Database_xml | – sequence: 1 dbid: DOA name: DOAJ Directory of Open Access Journals url: https://www.doaj.org/ sourceTypes: Open Website – sequence: 2 dbid: 8FG name: ProQuest Technology Collection url: https://search.proquest.com/technologycollection1 sourceTypes: Aggregation Database |
DeliveryMethod | fulltext_linktorsrc |
Discipline | Engineering |
EISSN | 1687-5974 |
Editor | Tuo Han |
Editor_xml | – fullname: Tuo Han |
ExternalDocumentID | oai_doaj_org_article_4f2e1608ec9344f1841fab029011f313 A819950098 10_1155_ijae_7720612 |
GroupedDBID | 0R~ 188 24P 29J 2UF 2WC 4.4 5GY 5VS 8FE 8FG 8R4 8R5 AAFWJ AAJEY AAYXX ABDBF ABJCF ABUWG ACCMX ACIWK ACUHS ADBBV ADMLS AEGXH AENEX AFKRA AFPKN AINHJ ALMA_UNASSIGNED_HOLDINGS ARAPS BCNDV BENPR BGLVJ BPHCQ C1A CCPQU CITATION CS3 CWDGH E3Z EBS EJD ESX GROUPED_DOAJ H13 HCIFZ I-F IAO IEA IL9 ISR ITC KQ8 L6V M7S MK~ OK1 OVT P62 PHGZM PHGZT PIMPY PQQKQ PROAC PTHSS Q2X RHU RNS TR2 TUS UGNYK UNMZH ~8M M~E 7TB 8FD AAMMB AEFGJ AGXDD AIDQK AIDYY AZQEC DWQXO FR3 H8D L7M PKEHL PQEST PQGLB PQUKI PRINS PUEGO |
ID | FETCH-LOGICAL-c427t-91f75b756a8d896e780282db3a4c7f997c11f024fc60a347dfb4fe9477b2011e3 |
IEDL.DBID | BENPR |
ISSN | 1687-5966 |
IngestDate | Wed Aug 27 01:30:54 EDT 2025 Fri Jul 25 19:01:32 EDT 2025 Thu Apr 17 06:54:43 EDT 2025 Tue Apr 15 04:04:16 EDT 2025 Fri Apr 11 03:21:33 EDT 2025 Tue Jul 01 02:40:18 EDT 2025 |
IsDoiOpenAccess | true |
IsOpenAccess | true |
IsPeerReviewed | true |
IsScholarly | true |
Issue | 1 |
Language | English |
LinkModel | DirectLink |
MergedId | FETCHMERGED-LOGICAL-c427t-91f75b756a8d896e780282db3a4c7f997c11f024fc60a347dfb4fe9477b2011e3 |
Notes | ObjectType-Article-1 SourceType-Scholarly Journals-1 ObjectType-Feature-2 content type line 14 |
ORCID | 0009-0009-0641-1752 0009-0008-1532-125X 0009-0000-1641-3334 0009-0008-2521-0350 |
OpenAccessLink | https://www.proquest.com/docview/3144715493?pq-origsite=%requestingapplication% |
PQID | 3144715493 |
PQPubID | 237291 |
ParticipantIDs | doaj_primary_oai_doaj_org_article_4f2e1608ec9344f1841fab029011f313 proquest_journals_3144715493 gale_infotracmisc_A819950098 gale_infotracacademiconefile_A819950098 gale_incontextgauss_ISR_A819950098 crossref_primary_10_1155_ijae_7720612 |
ProviderPackageCode | CITATION AAYXX |
PublicationCentury | 2000 |
PublicationDate | 2024-12-02 |
PublicationDateYYYYMMDD | 2024-12-02 |
PublicationDate_xml | – month: 12 year: 2024 text: 2024-12-02 day: 02 |
PublicationDecade | 2020 |
PublicationPlace | New York |
PublicationPlace_xml | – name: New York |
PublicationTitle | International Journal of Aerospace Engineering |
PublicationYear | 2024 |
Publisher | John Wiley & Sons, Inc Wiley |
Publisher_xml | – name: John Wiley & Sons, Inc – name: Wiley |
References | e_1_2_8_16_2 e_1_2_8_17_2 e_1_2_8_18_2 e_1_2_8_19_2 e_1_2_8_12_2 e_1_2_8_23_2 e_1_2_8_13_2 e_1_2_8_24_2 e_1_2_8_14_2 e_1_2_8_15_2 Zhong Y. W. (e_1_2_8_8_2) 2015; 36 e_1_2_8_9_2 Zhong Y. W. (e_1_2_8_7_2) 2015; 27 e_1_2_8_2_2 e_1_2_8_1_2 Ren T. R. (e_1_2_8_4_2) 2010; 31 e_1_2_8_6_2 e_1_2_8_5_2 e_1_2_8_20_2 e_1_2_8_10_2 e_1_2_8_21_2 e_1_2_8_11_2 Nicolaides J. D. (e_1_2_8_3_2) 1953; 395 Reeves P. M. (e_1_2_8_22_2) 1974 |
References_xml | – ident: e_1_2_8_16_2 doi: 10.1103/PhysRevA.35.1795 – ident: e_1_2_8_10_2 doi: 10.1016/S0020-7462(96)00096-0 – ident: e_1_2_8_20_2 doi: 10.1016/j.ijnonlinmec.2023.104504 – volume: 31 start-page: 2082 year: 2010 ident: e_1_2_8_4_2 article-title: Coning motion analysis of spinning missile based on gyrodynamics publication-title: Journal of Astronautics – volume: 27 year: 2015 ident: e_1_2_8_7_2 article-title: Stability analysis of periodic solutions for nonlinear angle motion of projectiles and rockets publication-title: Journal of Ballistics – ident: e_1_2_8_23_2 doi: 10.2514/3.25343 – ident: e_1_2_8_18_2 doi: 10.1016/j.ymssp.2012.02.013 – ident: e_1_2_8_11_2 doi: 10.1016/j.taml.2022.100385 – ident: e_1_2_8_2_2 doi: 10.2514/3.50025 – ident: e_1_2_8_17_2 doi: 10.1016/S0266-8920(99)00031-4 – ident: e_1_2_8_19_2 doi: 10.1016/j.jsv.2023.118037 – volume: 395 year: 1953 ident: e_1_2_8_3_2 article-title: On the free flight motion of missiles having slight configurational asymmetries publication-title: Institute of the Aeronautical Sciences – volume: 36 start-page: 1195 year: 2015 ident: e_1_2_8_8_2 article-title: Hopf bifurcation analysis of nonlinear angular motion stability of projectile publication-title: Acta Armamentarii – volume-title: Development and application of a non-Gaussian atmospheric turbulence model for use in flight simulators, NASA Contractor Report NASA CR-2451 year: 1974 ident: e_1_2_8_22_2 – ident: e_1_2_8_6_2 doi: 10.1007/s11071-019-05159-3 – ident: e_1_2_8_12_2 doi: 10.1007/s11071-014-1310-8 – ident: e_1_2_8_15_2 doi: 10.1103/PhysRevA.28.3003 – ident: e_1_2_8_24_2 doi: 10.1016/j.strusafe.2015.11.001 – ident: e_1_2_8_1_2 doi: 10.21236/AD0442757 – ident: e_1_2_8_13_2 doi: 10.1007/s11071-016-3323-y – ident: e_1_2_8_21_2 doi: 10.1016/0096-3003(90)90003-L – ident: e_1_2_8_14_2 doi: 10.1007/s00707-013-1040-x – ident: e_1_2_8_5_2 doi: 10.1016/j.ast.2016.10.016 – ident: e_1_2_8_9_2 doi: 10.2514/1.A33864 |
SSID | ssj0060575 ssib005317291 |
Score | 2.2963476 |
Snippet | During flight, projectiles are subject to uncertainties such as aerodynamic forces, wind gusts, and measurement errors; all of which significantly affect their... |
SourceID | doaj proquest gale crossref |
SourceType | Open Website Aggregation Database Index Database |
SubjectTerms | Coordinate transformations Distribution (Probability theory) Methods Projectiles Random noise Systems stability Velocity |
SummonAdditionalLinks | – databaseName: DOAJ Directory of Open Access Journals dbid: DOA link: http://utb.summon.serialssolutions.com/2.0.0/link/0/eLvHCXMwrV1NTxsxELUqTvSACm1FaEBW1aqnVeL11_oICEgqgaK0SNws27ERCCUVSSR-PjP2LiIHxKXX3bG0frPjmdmdeUPID69mOrDAK6cYJCiM8apRw6aKioUUGojANfY7X16p0bX4fSNvXo36wpqwQg9cgBuIVEcGq2MwXIgECQlLzg_x9x9LPM-rrcHndclUOYMVRiFdmbuUg7t7FwcQR6I_33BAmaf_rdM4u5jzT2SnjQ3pcXmmXfIhzvfIx1eMgZ-Jm5aa1kg7NhG6SHRSPqeAgdPCQE7zOCN64dZLbJKkV4s7WHL2FFpGbporBegEwj86LoQRD_QyD5P-Qq7Pz_6ejqp2SkIVRK1XcFolLb2WyjWzxqioG0yjZp47EXQyBlTBEnjiFNTQcYA-eZGiEVp7dP6RfyVb88U87hNqAGljvBGzUAudlJMhgHuXUccEYZfvkZ8ddPZfIcOwOYmQ0iLEtoW4R04Q1xcZpLDOF0CxtlWsfU-xPfIdtWKRpGKOVTC3iJkd_5na4wYby5EKtUd-tUJpsXp0wbVNBbAf5LXakOxvSIIVhc3bnfJta8VLyyHb1Mhhxw_-x46-ke0aFJGLYeo-2Vo9ruMhhDQrf5Tf3me7v_FC priority: 102 providerName: Directory of Open Access Journals |
Title | Response Analysis of Projectile System Under Gaussian Noise Excitation Using Path Integral Method |
URI | https://www.proquest.com/docview/3144715493 https://doaj.org/article/4f2e1608ec9344f1841fab029011f313 |
Volume | 2024 |
hasFullText | 1 |
inHoldings | 1 |
isFullTextHit | |
isPrint | |
link | http://utb.summon.serialssolutions.com/2.0.0/link/0/eLvHCXMwfV3db9MwELdY9wIPiE9RGJWFQDxFreP4I09oG_0YUquqMLE3y3HsaRNqRttJPPG3c-c4Y32Al0SKHUW5s8-_O59_R8j7StbKMcczKxk4KIzxTMuRzrxkLjgNCFzheef5Qs7Oiy8X4iIF3LYprbKzidFQ143DGPmQA_JXyCfGP938zLBqFO6uphIaB-QQTLDWPXJ4Ml4sV_dHGKDHu6QPiegEXTAJU0sA0u9S4YUYXl1bPwSsiWv-3iIVufz_ZbHjMjR5Qh4n_EiPW4U_JQ_8-hl5dI9V8Dmxqzbv1dOOcYQ2gS7bkAsYAdqylNNY8ohO7e0WD1LSRXMFr4x_ucTaTWM2AV0CRKRnLanEDzqPBadfkPPJ-NvpLEuVFDJX5GoHFi0oUSkhra51Kb3S6GrVFbeFU6EsQV0swGodnBxZDuoJVRF8WShVIUDw_CXprZu1f0Vo6Zksy6osapcXKkgrnAMIILzyAaBZ1ScfOtGZm5Yww0RHQwiDIjZJxH1ygnK964M01_FBs7k0adaYIuTwuZH2ruRFEcAbZcFWI9z7ZYEz3ifvUCsGiSzWmClziTIzZ19X5ljj4XOkS-2Tj6lTaHYb62w6eAD_g9xXez2P9nrCTHP7zZ3yTZrpW_N3XL7-f_Mb8jAHEcdUmPyI9HabW_8WAM2uGpADPZkO0tiF--n3z9PZIIYH4Dr_Pf4DyGD1Yw |
linkProvider | ProQuest |
linkToHtml | http://utb.summon.serialssolutions.com/2.0.0/link/0/eLvHCXMwtV1LbxMxELZKOQAHxFMECliIitMq8fq1PiBUoGlCm6gqrdSb8XrtqghlS5IK-FP9jZ3x7pbmALde197X2OP5xp75hpC3paq0Z55nTjFwUBjjWaEGRRYU89EXgMA15jtPpmp0JL4cy-M1ctHlwmBYZbcmpoW6qj3ukfc5IH-NfGL8w9nPDKtG4elqV0KjmRa74c8vcNkW78efYXw383y4ffhplLVVBTIvcr0E7Y5alloqV1SFUUEX6HZUJXfC62gMfDqLYLmiVwPH4VNjKWIwQusSjWXg8Nxb5LbgYMkxM324c30-A1a9CjFRiIXQ4VOgyBL8ii7wXsr-6XcX-oBsEWGsmMRUOeBf9iEZveEDcr9Fq3SrmV4PyVqYPSL3rnEYPibuoImyDbTjN6F1pPvNBg8sObThRKepwBLdcecLTNuk0_oUbtn-7VuOcJpiF-g-AFI6bigsftBJKm_9hBzdiISfkvVZPQvPCDWBKWNKIyqfCx2Vk94D4JBBhwhAsOyRzU509qyh57DJrZHSoohtK-Ie-YhyveqDpNrpQj0_sa2OWhFzeN2gCN5wISL4viy6coAnzSxyxnvkDY6KRdqMGcblnKDM7Pjrgd0qMNUdyVl75F3bKdbLufOuTXOA_0GmrZWeGys9Qa_9anM3-LZdVxb2rxY8_3_za3JndDjZs3vj6e4LcjcHcacgnHyDrC_n5-ElQKll-SrNX0q-3bTCXAK9wiuK |
linkToPdf | http://utb.summon.serialssolutions.com/2.0.0/link/0/eLvHCXMwtV1LbxMxEB6VVEJwQDxFoICFqDitEq9fuweEWprQUBpFgUq9Ga9jV0UoW5JUwF_rr-vMPkpzgFuvu97XeMbzjXfmG4A3hZ4Zz71InOYYoHAukkz3syRo7qPPEIEbqnc-HOv9I_npWB1vwEVbC0Nple2aWC3Us9LTHnlPIPI3xCcmerFJi5jsDd-f_UyogxT9aW3badQqchD-_MLwbflutIdzvZ2mw8HXD_tJ02Eg8TI1K7T0aFRhlHbZLMt1MBmFILNCOOlNzHP8DB7Ri0Wv-07ga8dCxpBLYwpynEHgfW_BpqGoqAObu4PxZHpduxG5XiWcaEJGFP5pNGuFUUabhq9U7_S7Cz3EuYQ31hxk1UfgX96icoHD-3Cvwa5sp1a2B7AR5g_h7jVGw0fgpnXObWAt2wkrI5vU2z24ALGaIZ1V7ZbYR3e-pCJONi5P8ZLBb98whrMqk4FNEJ6yUU1o8YMdVs2uH8PRjcj4CXTm5Tw8BZYHrvO8yOXMp9JE7ZT3CD9UMCEiLCy6sN2Kzp7VZB22CnKUsiRi24i4C7sk16sxRLFdHSgXJ7axWCtjio_rZ8HnQsqIkTCPrujTf2ceBRddeE2zYolEY07qeEIys6MvU7uTUeE7UbV24W0zKJarhfOuKXrA7yHerbWRW2sj0cr9-ul28m2zyiztX5t49v_Tr-A2Gov9PBofPIc7KUq7yshJt6CzWpyHF4irVsXLRoEZfLtpm7kE5x8xHA |
openUrl | ctx_ver=Z39.88-2004&ctx_enc=info%3Aofi%2Fenc%3AUTF-8&rfr_id=info%3Asid%2Fsummon.serialssolutions.com&rft_val_fmt=info%3Aofi%2Ffmt%3Akev%3Amtx%3Ajournal&rft.genre=article&rft.atitle=Response+Analysis+of+Projectile+System+Under+Gaussian+Noise+Excitation+Using+Path+Integral+Method&rft.jtitle=International+journal+of+aerospace+engineering&rft.au=Wang%2C+Liang&rft.au=Li%2C+Xinyi&rft.au=Peng%2C+Jiahui&rft.au=Zhang%2C+Zhonghua&rft.date=2024-12-02&rft.pub=John+Wiley+%26+Sons%2C+Inc&rft.issn=1687-5966&rft.eissn=1687-5974&rft.volume=2024&rft_id=info:doi/10.1155%2Fijae%2F7720612&rft.externalDBID=HAS_PDF_LINK |
thumbnail_l | http://covers-cdn.summon.serialssolutions.com/index.aspx?isbn=/lc.gif&issn=1687-5966&client=summon |
thumbnail_m | http://covers-cdn.summon.serialssolutions.com/index.aspx?isbn=/mc.gif&issn=1687-5966&client=summon |
thumbnail_s | http://covers-cdn.summon.serialssolutions.com/index.aspx?isbn=/sc.gif&issn=1687-5966&client=summon |