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Theoretical investigation of the dynamic lateral stability characteristics of Douglas design No. 39C, an early version of the X-3 research airplaneContains results of calculations made to determine the neutral oscillatory stability boundaries, period and time to damp of the oscillatory mode, and motions following disturbances. The calculations were made for Mach numbers of 0.75 and 2.3 at an attitude of 35,000 feet and for the landing condition at sea level.
Document ID
19930085567
Acquisition Source
Legacy CDMS
Document Type
Other
Authors
Bennett, Charles V
Date Acquired
August 16, 2013
Publication Date
January 18, 1949
Report/Patent Number
NACA-RM-L8L31
Report Number: NACA-RM-L8L31
Accession Number
93R14857
Distribution Limits
Public
Copyright
Work of the US Gov. Public Use Permitted.
Keywords
STABILITY - LATERAL AND DIRECTIONAL - DYNAMIC
STABILITY, LATERAL - STATIC
DAMPING DERIVATIVES - STABILITY
FLYING QUALITIES

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