Transonic-Wind-Tunnel Investigation of the Effects of Lip Bluntness and Shape on the Drag and Pressure Recovery of a Normal-Shock Nose Inlet in a Body of Revolution

Author: Olstad, Walter B.
Year: 1956
Document Type: N/A
Series: NACA Research Memorandums
Report Number: NACA-RM-L56C28
Link: https://digital.library.unt.edu/ark:/67531/metadc62696/

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