NASA NTRS · 19980223624
Second-Order Slender-Body Theory-Axisymmetric Flow
Abstract
Slender-body theory for subsonic and supersonic flow past bodies of revolution is extended to a second approximation, Methods are developed for handling the difficulties that arise at round ends, Comparison is made with experiment and with other theories for several simple shapes.
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VanDyke, Milton D.. 1959-01-01. Second-Order Slender-Body Theory-Axisymmetric Flow. https://ntrs.nasa.gov/citations/19980223624
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