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Experimental Determination of the Damping in Roll and Aileron Rolling Effectiveness of Three Wings Having 2 Degree, 42 Degree and 62 Degree Sweepback
Document ID
19930081894
Acquisition Source
Legacy CDMS
Document Type
Other
Authors
Bennett, Charles V
Johnson, Joseph L
Date Acquired
August 16, 2013
Publication Date
May 1, 1947
Report/Patent Number
NACA-TN-1278
Report Number: NACA-TN-1278
Accession Number
93R11184
Distribution Limits
Public
Copyright
Work of the US Gov. Public Use Permitted.
Keywords
WORK CARRIED ON AT LAL
WIND TUNNEL TESTS - NACA - FREE-SPINNING (15')
WINGS, SWEPTBACK
AILERONS
DAMPING IN ROLL
ROLLING MOMENTS - WINGS, SWEPTBACK

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