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|Title:||Fluid dynamic means of varying the thrust vector from an axisymmetric nozzle / submitted by Steven Slavko Vidakovic.|
|Author:||Vidakovic, Steven Slavko|
|School/Discipline:||Dept. of Mechanical Engineering|
|Abstract:||This thesis describes a thrust vectoring nozzle (TVN) which produces a jet which may be deflected at angles in excess of 80o from the nozzle axis by fluid dynamic means, while maintaining total thrust efficiency of the order of 50%, or at 50o with an efficiency of the order of 70%. The thrust vectoring by fluid dynamic means is achieved by injecting secondary fluid at the nozzle throat and partially separating the primary jet causing it to deform.|
|Dissertation Note:||Thesis (Ph.D.)--University of Adelaide, Dept. of Mechanical Engineering, 1995|
Jet planes Thrust reversers.
Fluid dynamics (Space environment)
|Description:||Bibliography: leaves 190-212.|
xxiii, 240 leaves : ill. ; 30 cm.
|Provenance:||This electronic version is made publicly available by the University of Adelaide in accordance with its open access policy for student theses. Copyright in this thesis remains with the author. This thesis may incorporate third party material which has been used by the author pursuant to Fair Dealing exception. If you are the author of this thesis and do not wish it to be made publicly available or If you are the owner of any included third party copyright material you wish to be removed from this electronic version, please complete the take down form located at: http://www.adelaide.edu.au/legals|
|Appears in Collections:||Mechanical Engineering theses|
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|01front.pdf||563.87 kB||Adobe PDF||View/Open|
|02whole.pdf||14.11 MB||Adobe PDF||View/Open|
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