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Please use this identifier to cite or link to this item: https://scholarhub.balamand.edu.lb/handle/uob/4140
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dc.contributor.advisorJadayel, Oussama Chafiqen_US
dc.contributor.authorOmar, Zaki Alen_US
dc.date.accessioned2020-12-23T14:40:32Z-
dc.date.available2020-12-23T14:40:32Z-
dc.date.issued2018-
dc.identifier.urihttps://scholarhub.balamand.edu.lb/handle/uob/4140-
dc.descriptionIncludes bibliographical references (p. 79-82).en_US
dc.description.statementofresponsibilityby Zaki Al Omaren_US
dc.format.extentxiv, 85 p. :ill., tables ;30 cm +1 CD-Rom (4 3/4 in.)en_US
dc.language.isoengen_US
dc.rightsThis object is protected by copyright, and is made available here for research and educational purposes. Permission to reuse, publish, or reproduce the object beyond the personal and educational use exceptions must be obtained from the copyright holderen_US
dc.subject.lcshRockets (Aeronautics)en_US
dc.titleAerodynamic assessment of the baseline configuration of a rocket : theoretical and numericalen_US
dc.typeThesisen_US
dc.contributor.departmentDepartment of Mechanical Engineeringen_US
dc.contributor.facultyFaculty of Engineeringen_US
dc.contributor.institutionUniversity of Balamanden_US
dc.date.catalogued2018-06-07-
dc.description.degreeMS in Mechanical Engineeringen_US
dc.description.statusUnpublisheden_US
dc.identifier.OlibID184532-
dc.rights.accessrightsThis item is not approved for publication.en_US
dc.provenance.recordsourceOliben_US
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