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An Analysis of Surface Pressures and Aerodynamic Load Distribution over the Swept Wing of the Douglas D-558-II Research Airplane at Mach Numbers from 0.73 to 1.73
Document ID
19930090061
Acquisition Source
Legacy CDMS
Document Type
Other
Authors
Taillon, Norman V
Date Acquired
August 16, 2013
Publication Date
April 21, 1958
Report/Patent Number
NACA-RM-H58A30
Report Number: NACA-RM-H58A30
Accession Number
93R19351
Distribution Limits
Public
Copyright
Work of the US Gov. Public Use Permitted.

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