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Wind-tunnel investigation at low speed of the effect of varying the ratio of body diameter to wing span from 0.1 to 0.8 on the aerodynamic characteristics in pitch of a 45 degree sweptback-wing-body combination
Document ID
19930087992
Acquisition Source
Legacy CDMS
Document Type
Other
Authors
Johnson, Harold S
Date Acquired
August 29, 2013
Publication Date
November 30, 1953
Report/Patent Number
NACA-RM-L53J09a
Report Number: NACA-RM-L53J09a
Accession Number
93R17282
Distribution Limits
Public
Copyright
Work of the US Gov. Public Use Permitted.

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