Simulation of Spinning Missile Flow Fields Using U2NCLE
Author:
Affiliation:
1. Mississippi State University
Publisher
American Institute of Aeronautics and Astronautics
Link
http://arc.aiaa.org/doi/pdf/10.2514/6.2002-2797
Reference7 articles.
1. Efficient Generation of High-Quality Unstructured Surface and Volume Grids
2. An investigation of parallel implicit solution algorithms for incompressible flows on multielement unstructured topologies
3. Approximate Riemann solvers, parameter vectors, and difference schemes
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1. Aerodynamic Analysis of a Spinning Missile Using a High-Order Unstructured-Grid Scheme;Journal of Spacecraft and Rockets;2010-01
2. Aerodynamic Analysis of a Spinning Missile with Dithering Canards using a High Order Unstructured Grid Scheme;47th AIAA Aerospace Sciences Meeting including The New Horizons Forum and Aerospace Exposition;2009-01-05
3. Unsteady Navier-Stokes Simulations of a Canard-Controlled Missile Configuration;26th AIAA Applied Aerodynamics Conference;2008-06-14
4. Higher Order Variable Extrapolation for Unstructured Finite Volume RANS Flow Solvers;17th AIAA Computational Fluid Dynamics Conference;2005-06-06
5. Aerothermal Analysis of Turbine Blades Using an Unstructured Flow Solver-U2NCLE;38th AIAA Thermophysics Conference;2005-06-06
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