As part of a research program aimed at providing information on the high angle-of-attack characteristics of three-surface fighter concepts incorporating a close-coupled canard, an investigation is being conducted on two specific configurations based on the F-18 and F-15 designs. The study configurations are being subjected to a wide range of tests including wind-tunnel tests, dynamic model tests, and piloted simulation. This paper summarizes the results obtained to date in this study. High-alpha results in the areas of static stability, damping, and control characteristics are reviewed and some of the more significant aerodynamic phenomena are identified.
High angle-of-attack characteristics of three-surface fighter aircraft
Aerospace Sciences Meeting ; 1982 ; Orlando, FL
01.01.1982
Aufsatz (Konferenz)
Keine Angabe
Englisch
Advanced fighter-attack aircraft
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