Design and Analysis Aerospike Blunt Body at Hypersonic Speed

Design and Analysis Aerospike Blunt Body at Hypersonic Speed | Research Square window.SnipcartSettings = { analytics: { enabled: false } }; (function() { var accessVector = localStorage.getItem('access_vector') || ''; window.dataLayer = window.dataLayer || []; if (accessVector) { window.dataLayer.push({ user: { profile: { profileInfo: { snid: accessVector } } } }); } })(); (function(w,d,s,l,i){w[l]=w[l]||[];w[l].push({'gtm.start':new Date().getTime(),event:'gtm.js'});var f=d.getElementsByTagName(s)[0],j=d.createElement(s),dl=l!='dataLayer'?'&l='+l:'';j.async=true;j.src='https://www.googletagmanager.com/gtm.js?id='+i+dl;f.parentNode.insertBefore(j,f);})(window,document,'script','dataLayer','GTM-K279D39R'); Browse Preprints In Review Journals COVID-19 Preprints AJE Video Bytes Research Tools Research Promotion AJE Professional Editing AJE Rubriq About Preprint Platform In Review Editorial Policies Our Team Advisory Board Help Center Sign In Submit a Preprint Cite Share Download PDF Research Article Design and Analysis Aerospike Blunt Body at Hypersonic Speed Dr.MUZEER.S, Vinoth Kumar RR This is a preprint; it has not been peer reviewed by a journal. https://doi.org/ 10.21203/rs.3.rs-4072585/v1 This work is licensed under a CC BY 4.0 License Status: Posted Version 1 posted You are reading this latest preprint version Abstract Hypersonic vehicles have the drag and heating problem when they operate at high speeds, to avoid or minimize this problem, aero spikes are utilized. This investigation finds a solution for reducing the drag and heating. Using ANSYS fluent, designed an aero spike, which has flow around a blunt body at highpersonic Mach number 6 with angle of attack zero. It is analyses for L/D ratio of 1.5 and 2. The front of the body is replaced by an aero spike which has weak oblique shocks and well-built detached shock. This develops a circular region between shock and blunt body. This works as a streamlined profile to reduce heat as well as drag. Aeronautics and Astronautics Aero spike Blunt body Hypersonic Mach number ANSYS Bow shocks Full Text Additional Declarations The authors declare no competing interests. Cite Share Download PDF Status: Posted Version 1 posted You are reading this latest preprint version Research Square lets you share your work early, gain feedback from the community, and start making changes to your manuscript prior to peer review in a journal. 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Also discoverable on Platform About Our Team In Review Editorial Policies Advisory Board Help Center Resources Author Services Accessibility API Access RSS feed Manage Cookie Preferences © Research Square 2026 | ISSN 2693-5015 (online) Privacy Policy Terms of Service Do Not Sell My Personal Information {"props":{"pageProps":{"initialData":{"identity":"rs-4072585","acceptedTermsAndConditions":true,"allowDirectSubmit":true,"archivedVersions":[],"articleType":"Research Article","associatedPublications":[],"authors":[{"id":278192648,"identity":"dabf9dfb-25f2-4d67-b381-b5156c17ba84","order_by":0,"name":"Dr.MUZEER.S","email":"data:image/png;base64,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","orcid":"https://orcid.org/0000-0002-7962-6537","institution":"Sanjay Ghodawat University","correspondingAuthor":true,"prefix":"Dr.","firstName":"","middleName":"","lastName":"MUZEER.S","suffix":""},{"id":278192689,"identity":"e3c1e526-f8e4-4314-9eb7-24e3e6881685","order_by":1,"name":"Vinoth Kumar RR","email":"","orcid":"","institution":"Sanjay Ghodawat University","correspondingAuthor":false,"prefix":"","firstName":"Vinoth","middleName":"Kumar","lastName":"RR","suffix":""}],"badges":[],"createdAt":"2024-03-11 09:55:30","currentVersionCode":1,"declarations":{"humanSubjects":false,"vertebrateSubjects":true,"conflictsOfInterestStatement":false,"humanSubjectEthicalGuidelines":false,"humanSubjectConsent":false,"humanSubjectClinicalTrial":false,"humanSubjectCaseReport":false,"vertebrateSubjectEthicalGuidelines":true},"doi":"10.21203/rs.3.rs-4072585/v1","doiUrl":"https://doi.org/10.21203/rs.3.rs-4072585/v1","draftVersion":[],"editorialEvents":[],"editorialNote":"","failedWorkflow":false,"files":[{"id":52466856,"identity":"277e3f00-b0d7-41bf-9638-3bcd1df52c21","added_by":"auto","created_at":"2024-03-12 02:10:57","extension":"pdf","order_by":1,"title":"","display":"","copyAsset":false,"role":"manuscript-pdf","size":399865,"visible":true,"origin":"","legend":"","description":"","filename":"HYPERSONICSPEED.pdf","url":"https://assets-eu.researchsquare.com/files/rs-4072585/v1_covered_dcba6050-feea-4555-866c-fdf44f836df1.pdf"}],"financialInterests":"The authors declare no competing interests.","formattedTitle":"\u003cp\u003eDesign and Analysis Aerospike Blunt Body at Hypersonic Speed\u003c/p\u003e","fulltext":[],"fulltextSource":"","fullText":"","funders":[],"hasAdminPriorityOnWorkflow":false,"hasManuscriptDocX":false,"hasOptedInToPreprint":true,"hasPassedJournalQc":"","hasAnyPriority":true,"hideJournal":true,"highlight":"","institution":"","isAcceptedByJournal":false,"isAuthorSuppliedPdf":true,"isDeskRejected":"","isHiddenFromSearch":false,"isInQc":false,"isInWorkflow":false,"isPdf":true,"isPdfUpToDate":true,"isWithdrawnOrRetracted":false,"journal":{"display":true,"email":"[email protected]","identity":"researchsquare","isNatureJournal":false,"hasQc":true,"allowDirectSubmit":true,"externalIdentity":"","sideBox":"","snPcode":"","submissionUrl":"/submission","title":"Research Square","twitterHandle":"researchsquare","acdcEnabled":true,"dfaEnabled":false,"editorialSystem":"","reportingPortfolio":"","inReviewEnabled":false,"inReviewRevisionsEnabled":true},"keywords":"Aero spike, Blunt body, Hypersonic Mach number, ANSYS, Bow shocks","lastPublishedDoi":"10.21203/rs.3.rs-4072585/v1","lastPublishedDoiUrl":"https://doi.org/10.21203/rs.3.rs-4072585/v1","license":{"name":"CC BY 4.0","url":"https://creativecommons.org/licenses/by/4.0/"},"manuscriptAbstract":"\u003cp\u003eHypersonic vehicles have the drag and heating problem when they operate at high speeds, to \u0026nbsp;avoid or minimize this problem, aero spikes are utilized. This investigation finds a solution for \u0026nbsp;reducing the drag and heating. Using ANSYS fluent, designed an aero spike, which has flow \u0026nbsp;around a blunt body at highpersonic Mach number 6 with angle of attack zero. It is analyses for \u0026nbsp;L/D ratio of 1.5 and 2. The front of the body is replaced by an aero spike which has weak oblique \u0026nbsp;shocks and well-built detached shock. This develops a circular region between shock and blunt \u0026nbsp;body. 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