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Second-Order Slender-Body Theory-Axisymmetric FlowSlender-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.
Document ID
19980223624
Acquisition Source
Headquarters
Document Type
Other - NASA Technical Report (TR)
Authors
VanDyke, Milton D. (NASA Ames Research Center Moffett Field, CA United States)
Date Acquired
September 6, 2013
Publication Date
January 1, 1959
Subject Category
Fluid Mechanics And Heat Transfer
Report/Patent Number
NASA-TR-R-47
Report Number: NASA-TR-R-47
Distribution Limits
Public
Copyright
Work of the US Gov. Public Use Permitted.

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