Stability and control problems which result from inertia coupling during roll maneuvers is of particular concern in design of fighter and interceptor aircraft, where high rolling rate and large amplitude roll maneuvers are critically required; important aircraft design implications resulting from consideration of this type of maneuver.
Airplane design implications of inertia coupling problem
Aeronautical Eng Rev
Aeronautical Engineering Review ; 16 , n 9
1957
6 pages
Article (Journal)
English
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