STOL Tactical Aircraft Investigation, Externally Blown Flap. Volume 5. Part 3. Stability and Control Derivative Accuracy Requirements and Effects of Augmentation System Design
Abstract
Contents: Flying qualities requirements; Selection of baseline flight condition; Selection of coefficient variation ranges; Technical approach; Coefficient prediction accuracy requirements; Lateral-directional parameter variation data; Longitudinal parameter variation data; Coefficient accuracy requirements -- unaugmented aircraft; Coefficient accuracy requirements -- baseline augmented aircraft.
Document Details
- Document Type
- Technical Report
- Publication Date
- Apr 01, 1973
- Accession Number
- AD0767182
Entities
People
- Victor H. Okumoto
- William K. Elsanker