Recovery Techniques for Aircraft in Spinning Flight.
AIR FORCE INST OF TECH WRIGHT-PATTERSON AFB OH SCHOOL OF ENGINEERING
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This study represents an attempt to use numerical solutions of the equations of motion to discover the most effective control surface deflections for use in a delta-winged fighter for recovery from a fully developed spin. The recovery methods were tested upon stable spins since the stable flat spin is generally the most dangerous spin.
- Attack and Fighter Aircraft