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- W327637618 abstract "Abstract : Computational fluid dynamics (CFD) predictions of static aerodynamic coefficients for large caliber (120-mm) M829-like cone-cylinder-flare kinetic energy (KE) projectile shapes are presented. Zero-yaw drag and static pitch- plane aerodynamic coefficients are presented for velocities in the range 1.5 to 3.0 km/sec for several flare angles. The aerodynamic coefficients are required to assess the velocity retardation and static stability of candidate configurations that use the M829 projectile as a basis for design. Comparisons of the aerodynamic coefficients are made with those of the fielded M829 projectile, and a preliminary evaluation is made of the performance of these shapes in hypersonic flight. Computational fluid dynamics, Supersonic flow, Kinetic energy projectiles, Aerodynamics." @default.
- W327637618 created "2016-06-24" @default.
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- W327637618 date "1994-09-01" @default.
- W327637618 modified "2023-09-23" @default.
- W327637618 title "Static Aerodynamics CFD Analysis for 120-mm Hypersonic KE Projectile Design" @default.
- W327637618 hasPublicationYear "1994" @default.
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