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Pressure distribution on fuselage of airplane modelThe method of determining the pressure distribution on the fuselage is described, with special attention to how it is affected by the presence of the wings.
Document ID
19930086653
Acquisition Source
Legacy CDMS
Document Type
Other
Date Acquired
September 6, 2013
Publication Date
February 1, 1925
Report/Patent Number
NACA-TM-300
Report Number: NACA-TM-300
Accession Number
93R15943
Distribution Limits
Public
Copyright
Work of the US Gov. Public Use Permitted.
Keywords
FUSELAGES - PRESSURE DISTRIBUTION (WIND TUNNEL)
PRESSURE DISTRIBUTION - FUSELAGES - FOKKER F 3

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