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FIN DAMAGE AND MASS OFFSET FOR KINETIC ENERGY PROJECTILE SPIN/PITCH LOCK-IN
A study and a general model for the roll/pitch frequency lock-in phenomenonare made for long antitank kinetic energy projectiles and missiles in general to quantify the necessary projectileExpand
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Viscous Compressible Flow in the Boundary Region of an Axial Corner
Laminar flow along a 90-deg corner, formed by the intersection of two semi-infinite flat plates, is analyzed, under the assumption of shock-free supersonic flow. The analysis is based on the methodExpand
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Autism spectrum disorders: Update of evaluation and treatment
Autistic spectrum disorders are a group of neuro-developmental conditions that are increasingly capturing the attention of clinicians and investigators. New insights from genetics andExpand
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Spike-nosed projectiles - Computations and dual flow modes in supersonic flight
Abstract : This study was made to assess the capability of a Computational Fluid Dynamic (CFD) method to adequately determine the aerodynamic coefficients for the unusual configurations ofExpand
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Sabot opening lift force - Analysis, CFD, and test
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Assessment of two fast aerodynamic codes for guided projectiles
Two fast missile aerodynamic prediction codes, the NSWCAP and Missile DATCOM, have been applied to the geometry of the guided, gun-launched Copperhead projectile. The two codes are evaluated inExpand
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Anti-Tank Spike-Nosed Projectiles With Vortex Rings: Steady and Non- Steady Flow Simulations
Abstract : Numerical computations are reported for a spike-nosed projectile configuration with a vortex generator ring. A new vortex-dominated flow field is computed at supersonic speeds of M - 3.5,Expand
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Flow Simulation and Drag Components for HEAT Projectiles with Spike and Cone Noses.
Abstract : Seven computations are reported for the two classes of projectile configurations of shaped charge antitank projectiles. The first class is of spiked nose with vortex generator ring,Expand
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