The prediction of aerodynamic force and moment coefficients on elliptic cone bodies at both angle of attack and sideslip by use of Newtonian impact theory

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dc.contributor.authorWells, William R.en
dc.contributor.committeechairHassan, Hassan A.en
dc.contributor.committeememberTruitt, Robert W.en
dc.contributor.departmentAeronautical Engineeringen
dc.date.accessioned2014-03-14T21:45:13Zen
dc.date.adate2012-09-08en
dc.date.available2014-03-14T21:45:13Zen
dc.date.issued1961-05-05en
dc.date.rdate2012-09-08en
dc.date.sdate2012-09-08en
dc.description.abstractNewtonian theory was applied, in this analysis, to the elliptic cone segment at angles of attack and sideslip. Closed form expressions for the aerodynamic coefficients and static stability derivatives were obtained. Expressions for the full and half conic bodies were given and approximate expressions were given for the half cone case. The circular cone results were obtained as a special case of the general results. Comparisons of the theoretical calculations with experimental results at hypersonic speeds were made of the aerodynamic coefficients and static derivatives for several conic segments. Generally, good agreement was observed for specified ranges of fineness ratios and angles of attack.en
dc.description.degreeMaster of Scienceen
dc.format.extent57 leavesen
dc.format.mediumBTDen
dc.format.mimetypeapplication/pdfen
dc.identifier.otheretd-09082012-040433en
dc.identifier.sourceurlhttp://scholar.lib.vt.edu/theses/available/etd-09082012-040433/en
dc.identifier.urihttp://hdl.handle.net/10919/44672en
dc.language.isoenen
dc.publisherVirginia Techen
dc.relation.haspartLD5655.V855_1961.W455.pdfen
dc.relation.isformatofOCLC# 26969858en
dc.rightsIn Copyrighten
dc.rights.urihttp://rightsstatements.org/vocab/InC/1.0/en
dc.subject.lccLD5655.V855 1961.W455en
dc.subject.lcshAerodynamic loaden
dc.subject.lcshDrag (Aerodynamics)en
dc.subject.lcshLift (Aerodynamics)en
dc.subject.lcshNewtonian telescopesen
dc.titleThe prediction of aerodynamic force and moment coefficients on elliptic cone bodies at both angle of attack and sideslip by use of Newtonian impact theoryen
dc.typeThesisen
dc.type.dcmitypeTexten
thesis.degree.disciplineAeronautical Engineeringen
thesis.degree.grantorVirginia Polytechnic Instituteen
thesis.degree.levelmastersen
thesis.degree.nameMaster of Scienceen

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