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INVESTIGATION OF STATIC PRESSURES AND BOUNDARY-LAYER CHARACTERISTICS ON THE FORWARD PARTS OF NINE FUSELAGES OF VARIOUS CROSS-SECTIONAL SHAPES AT M INFINITY EQUAL 2.01Boundary layer characteristics of fuselages of various cross sectional shapes at static pressure
Document ID
19630002657
Acquisition Source
Legacy CDMS
Document Type
Other - NACA Research Memorandum
Authors
Hasel, L. E. (NASA Langley Research Center Hampton, VA, United States)
Kouyoumjian, W. L. (NASA Langley Research Center Hampton, VA, United States)
Date Acquired
August 1, 2013
Publication Date
January 21, 1957
Subject Category
Aircraft
Report/Patent Number
NACA-RM-L56I13
Accession Number
63N12533
Distribution Limits
Public
Copyright
Work of the US Gov. Public Use Permitted.
Keywords
FUSELAGE
STATIC PRESSURE
BOUNDARY LAYER

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