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The Rolling Moment Due to Sideslip of Triangular, Trapezoidal, and Related Plan Forms in Supersonic Flow
Document ID
19930082386
Acquisition Source
Legacy CDMS
Document Type
Other
Authors
Jones, Arthur L
Spreiter, John R
Alksne, Alberta
Date Acquired
August 16, 2013
Publication Date
October 1, 1948
Report/Patent Number
NACA-TN-1700
Report Number: NACA-TN-1700
Accession Number
93R11676
Distribution Limits
Public
Copyright
Work of the US Gov. Public Use Permitted.
Keywords
WINGS, RECTANGULAR
ROLLING MOMENTS - EFFECT OF SIDESLIPPING
ROLLING MOMENTS - WINGS
WINGS, TRAPEZOIDAL
LOAD DISTRIBUTION - WINGS
WINGS, SWEPTBACK
WINGS, DELTA
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