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Tactical Missile Aerodynamics: Prediction Methodology
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TLDR
The component build-up method for engineering analysis of Missiles at low-to-high Angles of Attack (AOA) analysis is described in this article, along with experiments for Missiles with noncircular Fuselages Vortex Cloud Model for Body Vortex Shedding and Tracking Panelling.Abstract:
Tactical Missile Drag Drag Prediction Methods for Axisymmetric Missile Bodies Introduction to the Aerodynamic Heating Analysis of Supersonic Missiles The Component Build-Up Method for Engineering Analysis of Missiles at Low-to-High Angles of Attack Analysis Methods and Experiments for Missiles with Noncircular Fuselages Vortex Cloud Model for Body Vortex Shedding and Tracking Panelling Methods with Vorticity Effects and Corrections for Nonlinear Compressibility Supersonic Full-Potential Methods for Missile Body Analysis Space Marching Euler Solvers Time-Asymptotic Euler/Navier-Stokes Methods for Subsonic/Transonic Flows Three-Dimensional Boundary Layers on Missiles Navier-Stokes Analyses of Flows over Slender Airframes Exhaust Plumes and Their Interaction with Missile Airframes - a New Viewpointread more
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Aerodynamic Analysis of Grid-Fin Configurations at Supersonic Speeds
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Hydrodynamic modeling of LMRS unmanned underwater vehicle and tow tank test validation
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An Aerodynamic and Static-Stability Analysis of the Hypersonic Applied Research Technology (HART) Missile
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ReportDOI
A New Approach to Aeroelastic Response, Stability and Loads of Missiles and Projectiles
TL;DR: In this article, a computer code for the dynamic stability, structural dynamics and aeroelastic response of the missile has been written using a geometrically exact, mixed finite element method.