Early flights indicated tendency for airplane to "Dutch Roll" at lower indicated air speeds; elimination of this condition accomplished by use of servomechanism termed "yaw damper"; method of analysis based upon airplane inverse frequency response characteristics has been used, from which airplane stability has been obtained.
Investigation of lateral dynamic stability in XB-47 airplane
J Aeronautical Sciences
Journal of the Aeronautical Sciences ; 17 , n 3
1950
16 pages
Article (Journal)
English
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Proportioning the airplane for lateral stability
NTRS | 1976
|Engineering Index Backfile | 1959
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