02.1 - Aerodynamics - CFD Methods and ValidationFIGHTER AIRCRAFT HIGH AOA DIRECTIONAL STABILITY IMPROVEMENT DESIGNK.-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. Sorry, there is no file available for this paper. |