Method based on superposition of results of potential theory and viscous force on cylindrical body due to transverse component of flow; application to aerodynamic design of aircraft rockets.
Estimation of normal-force, drag, and pitching-moment coefficients for blunt-based bodies of revolution at large angles of attack
J Aeronautical Sciences
Journal of the Aeronautical Sciences ; 21 , n 8
1954
Article (Journal)
English
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Transient ablation of blunt bodies at angles of attack
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