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STOL Tactical Aircraft Investigation - Externally Blown Flap Volume V Flight Control Technology Part III Stability and Control Derivative Accuracy Requirements and Effects of Augmentation System Design
Author(s): Elsanker, W. K., Okomoto, V. H.
Corporate Author(s): Rockwell International Corporation
Laboratory: Air Force Flight Dynamics Laboratory
Date of Publication: 1973-04
Report number: AFFDL TR 73-20 Volume 5 Part 3

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