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![AFFDLTR73-020volume05part03.pdf application/pdf thumbnail](https://digital2.library.iit.edu/files//medium/297a0817d00e2411aa2fd1f8d0d7a49b12348e3c.jpg)
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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
![AFFDLTR73-020volume05part02.pdf application/pdf thumbnail](https://digital2.library.iit.edu/files//medium/014fa96b891a4fda5ed3cae1be0db020ba71f53c.jpg)
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STOL Tactical Aircraft Investigation - Externally Blown Flap Volume V Flight Control Technology Part II Simulation Studies/Flight Control System Validation
Author(s): Campbell, J. E., Okomuto, V. H., Elsanker, W. K.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 2
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