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

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Report Number: AFFDL TR 73-20 Volume 5 Part 3
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
Pages: 202
Contract: F33615-71-C-1760
DoD Project: 643A
Identifier: AD0767182

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Provenance: AFRL/VACA

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