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Wind-tunnel corrections at high subsonic speeds particularly for an enclosed circular tunnelA review of existing publications on wind-tunnel corrections is followed by an approximate method for determining the corrections due to model and wake displacement and to lift. Relations are investigated for fuselages and wings of various spans in closed circular tunnels. A comparison is made between the computations and the tests in the DVL high-speed wind tunnel.
Document ID
19930093930
Acquisition Source
Legacy CDMS
Document Type
Other
Authors
Gothert, Bernhard Hermann
Date Acquired
August 16, 2013
Publication Date
February 1, 1952
Report/Patent Number
NACA-TM-1300
Report Number: NACA-TM-1300
Accession Number
93R23256
Distribution Limits
Public
Copyright
Work of the US Gov. Public Use Permitted.
Keywords
WIND TUNNELS
FLOW, SUBSONIC

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