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

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.

Subject Categories:

  • VSTOL

Distribution Statement:

APPROVED FOR PUBLIC RELEASE