Unsteady Navier-Stokes Simulations of a Canard-Controlled Missile Configuration
Author:
Affiliation:
1. Mississippi State University
Publisher
American Institute of Aeronautics and Astronautics
Link
http://arc.aiaa.org/doi/pdf/10.2514/6.2008-7324
Reference13 articles.
1. An investigation of parallel implicit solution algorithms for incompressible flows on multielement unstructured topologies
2. Characteristic Variable Boundary Conditions for Arbitrary Mach Number Algorithm in Rotating Frame
3. Unsteady Simulations of Bell-Agusta 609 Rotor Undergoing Higher Harmonic Oscillation
4. Full Annulus Simulation of a High-Speed Centrifugal Compressor Using an Unstructured RANS Flow Solver
5. Aerothermal Analysis of Turbine Blades Using an Unstructured Flow Solver-U2NCLE
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1. Magnus Effect over Aerodynamic Components of Spinning Missile;International Journal of Aeronautical and Space Sciences;2022-03-22
2. CFD Validation of Interaction of Fin Trailing Vortex with Downstream Control Surface in High Subsonic Flow;54th AIAA Aerospace Sciences Meeting;2016-01-02
3. Aerodynamic Analysis of a Spinning Missile Using a High-Order Unstructured-Grid Scheme;Journal of Spacecraft and Rockets;2010-01
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