Accession Number:
AD0767182
Title:
STOL Tactical Aircraft Investigation, Externally Blown Flap. Volume 5. Part 3. Stability and Control Derivative Accuracy Requirements and Effects of Augmentation System Design
Descriptive Note:
Final rept. 10 Jun 1971-10 Dec 1972
Corporate Author:
ROCKWELL INTERNATIONAL LOS ANGELES CA LOS ANGELES AIRCRAFT DIV
Personal Author(s):
Report Date:
1973-04-01
Pagination or Media Count:
201.0
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.
Descriptors:
Subject Categories:
- VSTOL