Aerodynamic Analysis of a Spinning Missile Using a High-Order Unstructured-Grid Scheme
Author:
Affiliation:
1. Mississippi State University, Mississippi State, Mississippi 39762
Publisher
American Institute of Aeronautics and Astronautics (AIAA)
Subject
Space and Planetary Science,Aerospace Engineering
Link
https://arc.aiaa.org/doi/pdf/10.2514/1.42988
Reference24 articles.
1. An Aerodynamic Analysis of a Spinning Missile with Dithering Canards
2. Aerodynamic Analysis of a Spinning Missile with Dithering Canards
3. Simulation of Spinning Missile Flow Fields Using U2NCLE
4. Numerical Simulation of a Spinning Missile with Dithering Canards Using Unstructured Grids
5. A sliding interface method for unsteady unstructured flow simulations
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1. CFD Validation of Interaction of Fin Trailing Vortex with Downstream Control Surface in High Subsonic Flow;54th AIAA Aerospace Sciences Meeting;2016-01-02
2. Numerical Analysis of Static and Dynamic Performances of Grid Fin Controlled Missiles;Journal of Spacecraft and Rockets;2015-07
3. Numerical analysis of static and dynamic performances of grid fin controlled missiles;32nd AIAA Applied Aerodynamics Conference;2014-06-13
4. The prediction of axial aerodynamic coefficient reduction using base bleed;Aerospace Science and Technology;2013-12
5. Evaluation and optimization of strapdown velocity numerical integration algorithms for SINS in spinning ballistic missiles;Journal of Central South University;2013-04
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