Effects of Exit Nozzle Diameter on Compressible Vortex Rings Flow Structure
47th AIAA Aerospace Sciences Meeting and the New Horizons Forum and Aerospace Exhibit 2009 ; 2009 ; Orlando, FL
47th AIAA Aerospace Sciences Meeting and the New Horizons Forum and Aerospace Exhibit 2009 ; 4626-4640
2009-01-01
15 pages
Includes bibliographical references and index; Also contains papers from the New Horizons Forum and Aerospace Exhibit 2009
Conference paper
English
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Analysis of the Flow Dynamics of Compressible Vortex Rings Using Compressible Gases
British Library Conference Proceedings | 2009
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