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Numerical Investigation of Aerodynamics of Canard-controlled Missile Using Planar and Grid Tail Fins
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Viscous computational fluid dynamic simulations were used to predict the aerodynamic coefficients and flow field around a canard-controlled missile in subsonic
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Numerical Investigation of Aerodynamics of Canard-Controlled Missile Using Planar and Grid Tail Fins
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Viscous computational fluid dynamic simulations were used to predict the aerodynamic coefficients and flowfield around a generic canard-controlled missile confi
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This book presents selected papers presented in the Symposium on Applied Aerodynamics and Design of Aerospace Vehicles (SAROD 2018), which was jointly organized
