An Experimental and Numerical Investigation of Swirling Flows in a Rectangular Nozzle

An Experimental and Numerical Investigation of Swirling Flows in a Rectangular Nozzle

<p>The high thrust to weight ratios now possible for military aircraft have made thrust vector pitch control more attractive and versatile than aerodynamic surface pitch control. Use of a rectangular nozzle is a natural consequence because articulation and sealing problems are less formidable...

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Bibliographic Details
Main Author: Sobota, Thomas Henry
Format: Others
Language:en
Published: 1987
Online Access:https://thesis.library.caltech.edu/881/1/Sobota_th_1987.pdf
Sobota, Thomas Henry (1987) An Experimental and Numerical Investigation of Swirling Flows in a Rectangular Nozzle. Dissertation (Ph.D.), California Institute of Technology. doi:10.7907/dw4x-ex64. https://resolver.caltech.edu/CaltechETD:etd-03052008-091015 <https://resolver.caltech.edu/CaltechETD:etd-03052008-091015>

Internet

https://thesis.library.caltech.edu/881/1/Sobota_th_1987.pdf
Sobota, Thomas Henry (1987) An Experimental and Numerical Investigation of Swirling Flows in a Rectangular Nozzle. Dissertation (Ph.D.), California Institute of Technology. doi:10.7907/dw4x-ex64. https://resolver.caltech.edu/CaltechETD:etd-03052008-091015 <https://resolver.caltech.edu/CaltechETD:etd-03052008-091015>

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