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
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
Abstract:
The abstract for this report is either unavailable or has yet to be entered
Provenance: AFRL/VACA
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
Abstract:
The abstract for this report is either unavailable or has yet to be entered
Provenance: AFRL/VACA