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A theoretical investigation of the effect of yawing moment due to rolling on lateral oscillatory stability
Document ID
19930082416
Acquisition Source
Legacy CDMS
Document Type
Other
Authors
Johnson, Joseph L
Sternfield, Leonard
Date Acquired
August 16, 2013
Publication Date
October 1, 1948
Report/Patent Number
NACA-TN-1723
Report Number: NACA-TN-1723
Accession Number
93R11706
Distribution Limits
Public
Copyright
Work of the US Gov. Public Use Permitted.
Keywords
STABILITY, LATERAL - STATIC
YAWING MOMENTS
TANKS, FUEL - WING-TIP
AIRPLANES, FIGHTER - JET
WINGS, SWEPTBACK
OSCILLATIONS, LATERAL
DAMPING IN ROLL
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