columbus · 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

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

Title: 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
Date: 1973
Index Abstract: Coming Soon
Photo Quality: Not Needed
Report Number: AFFDL TR 73-20 Volume 5 Part 3
Creator: Elsanker, W. K.; Okomoto, V. H.
Corporate Author: Rockwell International Corporation
Laboratory: Air Force Flight Dynamics Laboratory
Extent: 202
Identifier: AD0767182
Access Rights: Approved for public release; distribution unlimited
Distribution Classification: 1
Contract: F33615-71-C-1760
DoD Project: 643A
DoD Task: None Given
DTIC Record Exists: Yes
Distribution Change Authority Correspondence: None
Report Availability: Full text available
Date Issued: 1973-04
Abstract: The abstract for this report is either unavailable or has yet to be entered
Provenance: AFRL/VACA
Type: report
Format: 1 online resource