02.1 - Aerodynamics - CFD Methods and Validation

FIGHTER AIRCRAFT HIGH AOA DIRECTIONAL STABILITY IMPROVEMENT DESIGN

K.-J. Lee, KAI, South Korea

fighter aircraft conceptual design study was perfomed. but initially designed configuration's lateral/directional stability in high angle of attack is not sufficient to the requred deign objective. So perfomed the Trade-off study was based on the CFD analysis to derive the lateral / directional stability improvement.

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