Detached Eddy Simulations and Reynolds-Averaged Navier- Stokes Calculations of a Spinning Projectile
Author:
Affiliation:
1. University of Minnesota, Minneapolis, Minnesota 55455
Publisher
American Institute of Aeronautics and Astronautics (AIAA)
Subject
Space and Planetary Science,Aerospace Engineering
Link
https://arc.aiaa.org/doi/pdf/10.2514/1.31935
Reference33 articles.
1. Viscous Flow over Spinning Cones at Angle of Attack
2. Computations of Magnus effects for a yawed, spinning body of revolution
3. Boundary layer over spinning blunt body of revolution at incidence including Magnus forces
4. Vortex model for Magnus forces at low speeds, spins, and angles
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