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The flow past a straight and a swept-wing-body combination and their equivalent bodies of revolution at Mach numbers near 1.0Tests utilizing the Schlieren method of flow photography have been conducted to provide a comparison of the complete flow fields past a straight and a swept-wing-body combination and the flow fields past their equivalent bodies of revolution at Mach numbers around 1.0. The results indicated that the shock growth and positions on the wing-body combinations were closely reproduced in the flow past the equivalent body.
Document ID
19930093724
Acquisition Source
Legacy CDMS
Document Type
Other
Authors
Lindsey, Walter F
Date Acquired
August 29, 2013
Publication Date
April 9, 1954
Report/Patent Number
NACA-RM-L54A28a
Report Number: NACA-RM-L54A28a
Accession Number
93R23016
Distribution Limits
Public
Copyright
Work of the US Gov. Public Use Permitted.

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