Navier-Stokes Computations for a Spinning Projectile from Subsonic to Supersonic Speeds-Reference-Cited by-同舟云学术

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Navier-Stokes Computations for a Spinning Projectile from Subsonic to Supersonic Speeds

Published:2003-06-21 Issue: Volume: Page:
ISSN:
Container-title:21st AIAA Applied Aerodynamics Conference
language:
Short-container-title:

Author:

Silton Sidra¹

Affiliation:

1. U.S. Army Research Laboratory

Publisher

American Institute of Aeronautics and Astronautics

Link

http://arc.aiaa.org/doi/pdf/10.2514/6.2003-3936

Reference16 articles.

1. Computations of projectile Magnus effect at transonic velocities

Cited by 6 articles. 订阅此论文施引文献订阅此论文施引文献，注册后可以免费订阅5篇论文的施引文献，订阅后可以查看论文全部施引文献

1. Dynamics Characterization of Missiles with Control Flaps Based on CFD;Advanced Materials Research;2014-08-28

2. Application of surface conformed linear mesh and data subdivision technique to a spinning projectile;Computers & Fluids;2013-12

3. Surface conformed linear mesh and data subdivision technique for large-scale flow simulation and visualization in Variable Intensity Computational Environment;Computers & Fluids;2013-07

4. Studies of the unsteady supersonic base flows around three afterbodies;Acta Mechanica Sinica;2009-03-24

5. Numerical Simulation of a Spinning Projectile Using Parallel and Vectorized Unstructured Flow Solver;Lecture Notes in Computational Science and Engineering;2008-02-04

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