Case Study

Assessment of Nose Shape & Taper on Aerodynamic Stability of Missiles

Assessment of Nose Shape & Taper on Aerodynamic Stability of Missiles

Pages 1 Pages

© 2014 Zeus Numerix Pvt Ltd Ph +91 20 64731511 contact@zeusnumerix.com VERTICAL: AEROSPACE & DEFENCE SERVICE: ENGINEERING SERVICES TECHNOLOGY: CFD ASSESSMENT OF NOSE SHAPE & TAPER ON AERODYNAMIC STABILITY OF MISSILES Our customer is engaged in development of strategic guided missile systems. These missiles will travel at hypersonic speeds with interception range up to 5000 Km. Such missiles do not feature control surfa

Join for free to read