This report is intended for use as a collection and analysis of diverse data gathering, empirical, and analytical approaches to the high angle of attack aircraft stability and control problem; as a compendium of several methods of defining aircraft departure and spin susceptibility; as a reference for spin definition and spin recovery enhancement; as a review of specifications, regulations, and design guides as they pertain to high angle of attack flight; and as a medium for expounding where tomorrow's high angle of attack investigative attention should focus. The design of safe, effective fighter aircraft in the high angle of attack combat environment is reaching a critical point. Accepted flying qualities design guidelines (necessary to establish stability and control requirements) must be established to address flight operations in the high angle of attack flight regime. Most of the research to date has focused on aircraft departure. Parameters/criteria to define desired high angle of attack flying qualities in the post-stall region (outside the realm of departure) are still unanswered.
Fundamentals and Methods of High Angle-of-Attack Flying Qualities Research
1988
228 pages
Report
Keine Angabe
Englisch
Aeronautics , Avionics , Aircraft , Angle of attack , Attack , Attack aircraft , Control , Fighter aircraft , Flight , Flight envelope , High angles , Optimization , Recovery , Regions , Requirements , Spinning(Motion) , Stability , Stalling , Warfare , Angle of attack indicators , Flight control systems , Aerodynamic stability
High angle of attack flying qualities criteria
AIAA | 1990
|Velocity dependence of high angle of attack longitudinal flying qualities criteria
Tema Archiv | 1991
|Velocity Dependence of High Angle of Attack Longitudinal Flying Qualities Criteria
SAE Technical Papers | 1991
|High-Angle-of-Attack Flying Qualities - An Overview of Current Design Considerations
SAE Technical Papers | 1979
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