This report entails a brief review of the derivation, application and implied limitations of the aircraft departure susceptibility criteria presented in the MIL-STD-1797A Flying Qualities Specification. To begin the discussion, the six degree-of-freedom rigid body aircraft equations-of-motion and aircraft stability concepts are reviewed, focusing on their application to determine the susceptibility of an aircraft to depart from controlled flight. A methodology is then suggested that allows a designer to determine the departure susceptibility of an aircraft configuration through the course of its design (up to and including flight test) with increasing levels of accuracy as the design progresses. Aircraft Departure Criteria, High Angle-of-Attack Equations-of Motion.
Investigation of Current and Proposed Aircraft Departure Susceptibility Criteria with Application to Future Fighter Aircraft
1990
196 pages
Report
Keine Angabe
Englisch
Aircraft , Aerodynamics , Aeronautics , Equations of motion , High angles , Angle of attack , Configurations , Flight , Focusing , Limitations , Methodology , Motion , Specifications , Test and evaluation , Mathematical analysis , Aircraft configurations , Aircraft departure criteria , Six degree of freedom rigid body aircraft , Aircraft stability , Controlled flight
MCAIR Design Philosophy for Fighter Aircraft Departure and Spin Resistance
SAE Technical Papers | 1979
|