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Aerodynamic Characteristics of Bodies at Supersonic Speeds: A Collection of Three PapersThe three papers collected here are: 'The Effect of Nose Shape on the Drag of Bodies of Revolution at Zero Angle of Attack.', 'Base Pressure on Wings and Bodies with Turbulent Boundary Layers', and 'Flow over Inclined Bodies'. The subject of the first paper is the drag of the nose section of bodies of revolution at zero angle of attack. The main object of the second paper is to summarize the prinicpal results of the many wind tunnel and free flight measurements of base pressure on both bodies of revolution and blunt trailing edge airfoils.
Document ID
20030067330
Acquisition Source
Langley Research Center
Document Type
Other - Collected Works
Date Acquired
September 7, 2013
Publication Date
November 9, 1951
Subject Category
Aerodynamics
Report/Patent Number
NACA-RM-A51J25
Distribution Limits
Public
Copyright
Work of the US Gov. Public Use Permitted.

Related Records

IDRelationTitle20030067332WorkBase Pressure on Wings and Bodies with Turbulent Boundary Layers20030067333WorkFlow Over Inclined Bodies20030067331WorkThe Effect of Nose Shape on the Drag of Bodies of Revolution at Zero Angle of Attack
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